SCIENTIFIC ABSTRACT V.M. FRIDLAND - I.G. FRIDLENDER

• Document Type: CREST
• Collection: Scientific Abstracts
• Document Number (FOIA) /ESDN (CREST): CIA-RDP86-00513R000513710017-6
• Release Decision: RIF
• Original Classification: S
• Document Page Count: 100
• Document Creation Date: November 2, 2016
• Document Release Date: June 13, 2000
• Sequence Number: 17
• Publication Date: December 31, 1967
• Content Type: SCIENTIFIC ABSTRACT

/'0 Z-
3(2);30(1) /11--J"/ PHASE I BOOK EXPLOITATION SOV/2059
Akademiya nauk SSSR. Pochvennyy Institut im. V. V. Dokuchayeva
Pochvennaya s"yemka; rukovodstvo po polevym lssledovanlyam i.
kartirovaniyu pochv (Soil Surveying; A Manual on Field Surveying
and Mapping of Soils) Moscow, Izd-vo AN SSSR, 1959. 346 p.
7,000 copies printed. Errata slip inserted.
Resp. Eds.: I.V. Tyurin, Academician, I. P. Gerasimov, Academician,
Ye. N. Ivanova, Professor, and V. A. Nosin, Candidate of Sciences;
Ed. of Publishing House: V. Ya. Markov; Tech. Ed.: I. F. Kuzlmin,
PURPOSE: This book is intended for students and practiLioners of
soil science and land utilization. It will also be of interest
to geographers and cartographers engaged in soil surveying and
mapping projects.
COVERAGE: This work on soil surveying was prepared by a group of
scientists of the Department of Soil Geography and Cartography
of the Pochvennyy institut AN SSSR (Soil Institute, AS USSR).
The book discusses the methods used in both general and special-
card 1/7

Soil Surveying (Cont.) SOV12059
Ch. 2. Preparatory Work in Various Types of Soil 'Surveys
Field Equipment and Supplies MM. Fridland) 16
Working out the schedule and method7 coaecti-d-r-~Md
systematization of materials of previous workS 17
The topographic control for a soil survey 18
The simplest geodetic instruments used in the field
soil survey 22
The working equipment of a soil scientist 28
Soil drills 31
Equipment for the field study of the chemical
properties of soil 40
General field equipment and the means of transportation 41
Ch. 3. M3thodology and Techniques of the Field Soil Survey
(V.A. Nosin and B.F. Petrov) 46
Studying the conditions of soil formation 46
The geomorphological characteristics of a region 46
Geologic structure, original and soil-forming rocks 54
Hydrogeological conditions 59
Card 3/7

Soil Surveying (Cont. ) SOV/2059
Compiling and finishing soil maps 128
Preparing the cartographic base 129
Making up tYe legend of a soil map 130
Plotting soil boundaries and supplementary symbols 135
The finishing (border details) of soil maps 136
Ch. 6. Using Aerial Photography in Mapping Soil Cover (M.S.
Simakova) 146
Types of aerial photography and the properties of aerial
photographs 146
Interpreting the soil cover from aerial photographs 153
Special features of work organization in soil mapping from
aerial photographic material 165
The selection of aerophotographic materials for soil
surveys of various scales 165
The working schedule In soil mapping from aerophatographic
materials 166
Bibliography for Part 1 169
Card 5/7

Ooil Surveying (Cont.
PART I I
SOV/2059
Ch. 1. "',oil Studies as 1-t(Aated to Land Use and Agricultural
Planning in-Kolkhozles and Sovkhozes (M.N. Malyshkin) 171
Ch. 2. The Soil-meliorative Land Studies for Irrigagion
Purposes (A.N. Rozanov) 190
Ch. 3. Soil Studies for Drainage Purposes (A.P. Petrov) 235
Ch. 4. Specific Features of' Soil Surveys for Forestry
Purposes (V.N. Smirnov) 263
Ch. 5. Soil Studies as Related to the Planning of the
Amelioration of Agricultural Forestry Work (A.A. 'Ife
Yerokhina) 287
Supplement:
1. Methods for studying the water-physical properties of soils
and ground,.-I.6?.V. t1stapov and S.I. Dolgov) 299
2. The determination oA- rock content in soil surveys
(A.P. Petrov) 335
Card 6/7

Soil Surveying (Cont.)
SOV/2059
3. Forms from the soil reoord book 341
AVAILABLEt Library of Congress
MM/dfh
7-22-59
Card 7/7

SOV/10-59-5-4/25
AUTHOR: FridLand4_V.M.
TITLE: On the Problem of Zonality Factors
PERIODICAL: Izvestiya Akademii nauk SSSR, Seriya geografiches-
kaya, 1959, Nr 5, pp 29-37
ABSTRACT: Fifty years of development of the science of natural
geographical zones, created by V.V. Dokuchayev, are
described in this article. According to Academician
A.A. Grigorlyev, the most important problem of the
principle of div4sion of the Earth into natural geo-
graphical zones is the definition of factors and. the
character of their influence on the formation of
these zones. The natural geographical conditions in
general, and those of separate zones in particular,
are the results of a lengthy historical development
and of the interaction of two groups of factoraq bio-
climatie and geologo-geomorphological. The influence
Card 1/2 of one of these groups of factors explains the inter-

SOV/10-59-5-4/25
On the Problem of Zonality Factors
nal heterogeneity of different geographical zones.
This brought about a further division of these zones
intDsubzones, provinces, etc. The author gLves a de-
tailed description of certain zones and of factors
which caused the origination of conditions specific
to these zones. He mentions the following scientists
who took part in the development of the science of na-
tural geographical zones: Ya.N. Afanas"yev, M.I. Budyko,
G.N. Vysotskiyq I.P. Gerasimov, K.D. GI-inka, S.A. Za-
kharov, N.N. Ivanoy. VoLo Komarov, Ye.V. Lavrenko, L.I.
Prasolov, N.N. Rozov, V.B. Sochava, G.M. Tumin, and
K.A. Ufimtseva. There is I map, 1 table and 25 Soviet
references.
ASSOCIATION: Pochvennyy institut AN SSSR (The Soil Insititute of the
AS USSR)
Card 2/2

FRIDLTAND, V. 14.
Vertical sonality of North Vietnam sails. Poefivovedonio
n0-11:8-18 N 159. (MIRA 13:4)
1. Pochvennyy Institut Im. V.V.Dakuchuyeva.
(Vietnam, North--Soils)

ANTIPOV-KARATATRY, I.N., skedemik, otv.red.; TYURIN, I.Y., glavnyy red.;
GORMOV, N.I., red.; VERIGINA, K.Y., red.; ZONN, S.T., red.;
IVAHOVA, Ye.11., red.; r"R ZIKHHAN, O.K.. red.; KONONOVA,
M.K., red.; LOBOVA, Te.V.. red.; HISIW5TIN, Ye.H., red.: ROB3.
A.A., red.; ROZANOV, A.N., red.; SOKOLOV, A.V,, red.; FRI194P,_
'Y.K., red.; SHUTALOY, S.A., red.; TIFIROV, A.L., red.izd-va;
KAKUNI, Te.T., tokhn.red.
(Reports of Soviet soil scientists to the 7th International
Congress in the U.S.A.) Dokledy sovetskikh pochvovedov k VII
Mezhdunarodnomu kongressu v SSU. Koskva, Izd-vo Akad.nauk SSSR,
1960. 467 P. (MIRA 13:10)
1. International Congress of Soil Science. 7th. 2. AN Tadzhik-
skoy SSR, (for Antipov-Karatayev). 3. Pochvennyy inatitut im. V.V.
Dokuchayeva Akademii nauk SSBR, Moskva (for Antipov-Xaratayev. Gorbunoy,
(Continued on next card)

ANTIPOV-KARATATEV, I.N.---(continued) Card 2.
Ivanova,,Kbnonova. RosanoT,,Yridland, Sokolov).. 4. Labomtoriya
lesovedenlya Akedemii nauk SSSR, Moskva (for Zonn). 3. Voesoyuznyy
nouchno-iosledovatellskiy institut udobreniy i agropochvovedeniya
Vseaoyuznoy ordens Lenina Akedemii sell skokhoz.rwuk imeni V.I.Lenina
i Instill"ut zemledeliya skademii sellskokhoz.nauk Belorusskoy SSR (for
Kedrov-Zikhmen). 6. Institut mikrobiologii Akademii nauk SSSR, Moskva
(for Miahustin). 7. Nauchnyy inatitut po udobreniyam i insaktofungi-
taidam im. Ta.V.Samoylova, Moskva (for Sokolov).
0oil research)

FRIDLAND, V..M..
"On The Red-Yellow Lateritic Soils Of Permanently Moist Tropical Forest".
report submitted for the 7th Congress of International Society of Soil Science
Madison, Wisconsin, 15-23 Aug 6o.

f
_714DLAND" V*NO.
S.vmposium on the genesis of soils in the U.S.A. Fochvovedenio no.6;
112-116 Je 160. (MIRA 1):11)
(United States-Soil formation)

.-, W, Vladimir Markovich; ZARANKIN, V.H.. red.izd-va; YWTMOVA,
IR14L
N.Y., tekha.red.; XAKUNIV TO.T., tekhn.red.
(Mature of North Vietnam] Priroda Severnogo T'etnama. KoskIra, 1,
bcd-vo Akad.nauk SSSR, 1961. 173 p. (MIRA 14:4)
(Vietnam. North-Physical geography)

SEREBRYANNYY, L.R.; CHEBOTAREVA, N.S.; FRIDLAND9 V.M.
New materials from German researchers on the paleogeography,
nary stratigraphys geomorpholovys and the geography of soils. 'Frt;dy
Kom.cbetv.per, no.26i169473 '61- (MIRA 15-3)
(Geology)

FRIDLAND, V.M.
Soils of hilly areas of North Vietnam. Fochvovedenie no.12:
57-74 D 161. (MIRA 16:3)
1. Pochvennyy institut im. V.V.Dokuchayeva.
(Vietnam, North-Soils)

FRIDLAND. V.M.
Two ways of the formation of laterite concretions. Dok1,AH &SSR
137 no.5iI202-1205 Ap 161. (NIERA 14:4)
1, Pochvennyy institut im. V.V.Dokuchayeva AN SSSR. Prbdstavleno
akademikom I.V.Tyurinym.
(Vietnam. Nortb-.Laterite)

LETUNOV, P.A., doktor sellkboz. nauk., otv. red.; IVXIOVA, Ye.N.,
doktor sellkhoz. nauk, red.; ROZOV, kand. geogr. nauk,
red.; FRIDLAIflD,A.U.-, kand. geol.-miner. nauk., red.; SHASHKO,
D.I., 0. or geogr. nauk, red.; SHUVAIDV, S.A., kand. geol.-
miner. nauk, red.; GERASIMOV, I.P., akad. red. kart; MARKOV)
V.Ya.,, red. izd-va; KASHINA, P.S., tekhn. red.; RYLINA, Yu.V..,
tekhn. red.
[Subdividing the territory of the U.S.S.R. into soil zones;
in connection with agricultural use of the land] Poclrvenno-
geograficheskoe raionirovanie SSSR (v sviazi a sellsko-
khoziaistvenrqm ispoltzovaniem zemell). Moskva, Izd-vo
Akad. nauk SSSR, 1962. 422 p. (MIRA 15:5)
1. Akademiya nauk SM. Sovet po izucheniyu proizvoditelli7kh
ail.
(Soils)

SOYOLOV, A.V., doktor sellkhoz. nauk, otv. red.; IVANOVAj Ye.N.p red.;
SIIUVALOV, S.A., red,; ROZOVI N.N., red.; IMSIR, V.A., red.;
FRIDLAND, V.M.,, red RARKOV, V.Ya., red. izd-va; FOLMVA~ T.P.p
(Agrochemical charactei-Istics of the soils of the soils of the
U.S.S.R.; White Russian S.S.R.s Latvian S.S.R., Lithuanian S.S.R.,
Estonian S.S.R., Karelian A.S.S.R., and the norhtern regions of
the European part of the R.S.F.S.R.]Agrokhimicheskaia kharakteri-
stika pochv SSSR; Belorusskaia SSR, Letviiskaia W., Litovskaia
SM., Estonskaia M. Karellskaia ASSR i severnye raiony LIvropei-
skoi chasti RSFSP. Iljoskva, Izd-vo Akad. nauk SSSR, 1962. 279 p.
(MIRA 15:12)
1e Akademiya nauk SSSR. FochvemVry institut imeni. V.V.Dokuchaye-ra.
2. Otdel geografii Pochvennogo instituta imeni V.V.Dokuchayeva
Akademii nauk SSSR (for Ivanoval Shuvalovs Rozov Nosin, FYidland).
(Russia, Northwestern-Soil chemistryi

FRIDUND V M _DOKUCHAYEV, V.11.
Soil surveys In North Viet-Nam and their role in the progress of
tropical farming."
Report submitted to the Conf. on the Application of Science and Technology
for the Benefit of the Less Developed Areas.
Genevaj, Switzerland 4-20 Febru=7 1963

FRIDLAND, V.M.
Laterites of North Vietnam. Kora vyvetr. no.41126-146 162,
(MIRA 1519)
1. Pochvennyy institut AN SSSR.
(Vietnam, North--Laterite)

MIDLANDp V. M.; KARAYEVA, Z. S.
00~~~
Orifin of acid salinized soils. Foobvovedenie no.7:77-81
J'1 62. (HIn 15: 10)
1, Poohvennyy inatitut imeni V. V. Dokuohayeva.
I
(Vistnazo North-Saline and alImli soils)

FRIDLAND V M
-Seminar on the soil map of Europe. Fochvovedenie no.2s106-108
F 163. (Europe--Soils--Maps) (MIRA 160)

FRIDLAND, V.M.
Weathering surfaces of North Vietnam, Kora vyvetro no.6t
241-257 163. (MIRA 17:9)
1. Pochvennyy institut imeni V.V. Pokuchayeva, Moskva.

IV4NOVA Ye.N.I_nl_pIA!p
0 2, V.M.
UsIng the nev eystam in the r;orm',a"L!.,7,n and muppln Of 6011.40
Ibchvovedenle no.6&21 TaI64 &IPU 170)

FRIDLAND, V.M.; DOROKHOVA, K.Ya.; ZHITKOVA , A.I.
Nature of the structure of humid tropical soils (Morth Vietnam).
Dokl. AN SSSR 154 no, 3:707-709 Ja 164. (MIRh 17:5)
1. Pochvennyy institut im. V.V.Dokuchayeva i Ministerstvo sell
skogo khozyaystva SSSR. Predstavleno a-kademikom I.P.Gerasimovym.

SOKOLOV, A.V., otv. red.; SHKONDE, E.1.p kand. nellkhoz. nauk,
otv, red. Prinimal uchastlye ASKINAZI) D.L. p
red.; TROITSKIY, A.I.,, retsenzent; FRIDLAND, V.M.)
retsenzent
(Agrochemical characteristics of soils in the U.S.S.R.;
the Transcaucasian Republics] Agrokhimicheskaia kharak-
teristiks. pochv SSSR; respubliki Zakavkazlia. Moskvaj
Nauka, 1965. 319 P. (MIRA 18%5)
1. Akademiya nauk SSSR. Pochvenrqy institut im. V.V.
Dokuchayeva. 2. Chlen-korrespondent AN SSSR (for Sokolov).

------------
nr,,~-*;!~ Z3 Ap
- - - . . . - -7'
.; :l--,,~ml, :t' C--nra,
J~.;" ',MlPA 58:6)
., - ' '
. In.-.t:tul- gecgrifil AN I ,

AVERKO-ANTONOVICH, L.A.; KIRPICHNIKOV, P.A.; ZARETSKIT, U.S.; FlUDLAND, V.M.;
PROKHOROV, V.S.; RASPOPOVA, L.V.; Prinimala uchastive: ZUBKOVA, T*P*
Production of colored thiokol oealing materials. Kauch. i rez. 4
no.9:20-23 165. (MIRA 18:10)
1. Kazanskiy khimiko-takhnalogictieskiy institut imeni S.M.Kirovit.

ROZOV, N.N.; FRIDLAND. V.M.
Problems of soil science In the works of Academician I.P. Gerasinov;
on the occasion of his 60th birthdayl 1905 - . Pochvovedenie no. 121
28-33 D 165 (mim 19:1)

FR I D, V . Yfi $ C,:-.: -. d " c C; "C' -- (di "L;) "'11,,.-:i- i-; c ~- -, (;:; 1 -. t -, - 1. if , ;: -
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o4 lid L 1 -~ ~ -t- .~! .1 ! I~ 11,:!7 r .
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AUT11ORi Fridland, V. Ya., Engineer 98-58-7-10/21
TITLE: Calculation of Elements of One-Sided Deposition (Rasch6t
elementov odnostoronnego namyva)
PERIODICAL: Gidrotekhnicheskoye stroitel'stv0,1958,Nr 7, pp 35-37(USSP,).
ABSTRACT: The author devised formulae which permit the calculation of
any given moment in the state and character of an alluvial
surface and the intensity of the deposition at any given
point. For the stream transporting capacity, the well kncwn
formula ia used: IQ = q 13
-
Y
ej
where P is the specific w ghted hard expenditure;
%_ specific pulp expenditure on the map of the deposition;
T_ transversal inclination of the map of the deposition;
T - coefficient, which depends on the granulometric ground
composition and on the specific pulp expenditure;
n - the power indicator which depends mainly on the gran-
ulometric composition of the ground. This indicator can
have different meanings. Gilbert, Shoklich, Yeyer-Peter,
N.V. Goncharov and others take n - 1.5; Vac-Dougall,I.I.
Levi, Ye.A. Gavrnshchenko (ref. 1) take n - 2. These mean-
Card 112 ings were based on observations of small weighted depositions

Calculation of Elements of One-Sided Deposition 98-56-7-101'21
in canals and rivers. In hydro-mechanization processes, the
indicator n will have much larger limits, as the ground
used for the depositions will not be homogeneous. All de-
vised formulae result from this basic formula. There are
5 Soviet references,
1. Rivers--Sedimentation--Theory
Card 212

KKHITARTAN. Art4shes Kelkonovich. Prinimali uchaetiye: RMIKOV, V.S.,
assistant; FRIDLAND, V.Ya., assistant; KISHCHUK, GeYa., assistant.
PISAPMKO, K. S., tekhn.red.
[HydriCulics and fundamentals of gas dynamics] Gidravlika i oanovy
gazodinamiki. Kiev, Goo.izd-vo tekhn.lit-ry USEM, 1959. 279 p.
(KMA 12:8)
1. Kafedra gidravliki XIYOVBkogo ordena Lenina politakhnichaskogo
instituta (for Kaksimov, Fridland).
(Hydraulics) (Aerodynamics)

10,15,oo
39592
S/263/62/000/011/012/022
1007/1207
AUTHOR: Mkhitaryan, A. M., Maksimov, V. S., Labinov, S. D. and Fridland-, V Ya
TITLE: Method for studying the boundary layer by means of an electric hot-wirc anemometer
PERIODICAL: Refcrativnyy zhurnal, otdel'nyy vypusk. 32. lzmeritcl'naya tckhnika, no. 11, 1962, 36,
abstract 32.11.275. In collection "Novyye mctody izinereniy i pribory dlya gidravlich.,
issled". M., AS USSR, 1961, 90-92
TEXT: The kievskiy politekhnichcskiy institut (Kiev Polytechnic Institute) designed a test stand for studying
the turbulent boundary layer in order to find optimum methods for its control. The distribution of velocity
in the jet cross-section and the turbulence spectra were investigated. Average velocities and fluctuations were
measured by means of the 3TAM-3A (ETAM-3A) electric hot-wire anommeter designed by tile VEL
Width of the nozzle wire was 19 micr. The average flow velocities were found from the current intensity
of the measuring bridge, and the degree of turbulence, from the readings of a C-95 (S-95) electrostatic voltmeter
connected to the amplificr output. Shape and frequency of fluctuations as well as their relative amplitude
were determined by means of a :)H-7 (E1-7) cathode-ray oscilloscope and recorded on a M 1710-2 (M PO-2)
oscillograph. Calibration was done by a reference Prandti-tube. A 500 c time marker was used for determining
Card 1/2

Method for studying the...
S/263/62/000/011/012/022
1007/1207
the frequency [Abstracter's note: of fluctuations); the measuring nozzle was moved by means of a screw-
coordinator provided with a vernier scale. Accuracy of nozzle setting was 0.005 mm and of mean velocity
measurements, 0.5%. The intensity of fluctuations was determined with an accuracy of 5 to 10%. A movable
element, fastened to the flume bottom and connected to piezoelectric weighing scales designed by the Institut
mckhaniki AN USSR (Inztitute of Mechanics, AS, UkrSSR) was used for determining the stresses on the
surface. The scales had the following design features: during measurement the crystal-bearing ring driven by
a special gear induces in the crystal an alternating voltage. Due to this method, distortions of measurement
results, caused by leakage of the charge from the crystal, can be avoided. The accuracy of scale readings is
I %. There are 3 references and I figure.
[Abstracter's note: Complete translation.]
Card 2/2

5 / 3.117/6 1/ooo/ ooli/o _i4
E-195/Ll.35
AUTHORS Mkhitaryan, A. M. , Maks imov, V. S. , -Fr i (11-iind. _N1. Ya.
and Labinov, S.D.
TITLE; An experimental investigation of flow in the initial
sections of a semi-bounded turbulent jet
PERIODICAL: Izvestiya vysshiMi uchebn)-kh zavede"iy, Aviatsiolinz.,yo.
telchnika, no.41 iq6i, ni-iig
TLXT: Most of the published experimental. and theoretical
ifork on submerged turbulent jets has been concerned with the main
part of the jets, which is characterised by flow under the
conditions of an enclosed boundary layer. The presence of
developed turbulent inter-mixing makes it possible to assume,
ifith an adequate degree of accuracy, a similarity of velocity
diagrams expressed in dimensionless coordinates. A more complex
problem is the study of the initial section of the jet, where the
above assumption would result in considerable errbrs. The
authors have carried out an experimental wind-tunnel study of the
flow of-semi-bounded, turbulent jet, flowing out. of a right-angle
Card 4/3-)

An experimental investigation of flow... S/147/61/ooo/oo4/olh/on
E194/El-35
nozzle into a prismatic trough. As a result of' this inv~:!stigation
it has been established that, along a length of more than tell
equivalent diameters (of the nozzle) and on 705' of tile width of
the frough, there exists a nucleus of constant velocities. III
addition, the boundary layer forming on tile bottom of tile trough
is equivalent to a boundary layer forming on a flat plate
subjected to a flow of an infinite stream. Ex2criments carried
out with the help of a hot wire anemometer showed that in the
nucleus of the stream the degree of turbulence remained constant
along the length and width of the trough. Finally, an empirical
relationship has been obtained, giving the location of the upper
limit of the nucleus of constant velocities in a sewi-bounded
jet.: Y/h = 0- x/h - a (8)
where: y is the flow coordinate of points of upper limit of
the nucleus of constant velocities; 11 is the height of tile
nozzle; a is a coefficient depending on the amount of
turbulence at the outlet from the nozzle, and equal in this
case to + 0.0108.
Card 2/3

An experii.iont:xI irvestigation of
There are 8 figures.
ASSOCIATION: Kafedra gidravliki,
(Department of Flydriiulics,
Ins t itlute)
SUBMITTED: January 16, 1961
... s/147/61/000/004/014/021
E195/E135
Kiyevskiy politekhnicheskiy instit.
Kiev Polytechnical
Card 3/3

27243
1~ 21 2-601 S/1 70/6~. 100410C91002101 3
B1 04/Bl 25
AUTHORS: Witaryan, A. M., Maksimov, V. S., Fridland, V. Ya.,
Labinov, S. D.
TITLE: Method of investigating the boundary layer in an operating pal".
of a new type
PERIODICAL: Inzhenerno-fizicheskiy zhurnal, v, 4, no. 9, 1961' 12-16
TEXT: The turbulent boundary layer of a body with a pressure gradient along
its axis and a gas jet flowing about it has been studied, The experiments
were performed because at present there is no complete theory available,
which would permit an exact calculation of the disrupture of the boundary
layer.. First of all, an operating part was developed, which produces a jet
with a long core of constant velocity. An attempt was made to obtain a
constant velocity, a constant static pressure, and a constant turbulence of
flow throughout the operating part. The authors determined the velocity
distribution over the cross section of the jet and also the turbulence
spectrum. The mean velocities and pressure pulsations were measured by an
electrothermoanemometer of the type 3TA*3A (ETA11-3A). Shape, frequency,
Card 1/ 3

27243
S/170/61/004/009/002/013
Method of investigating the B104/B125
and amplitude of oscillations were 7isually determined by means of a
cathode-ray oscilloscope and recorded on a film, First, the authors
measured the parameters of a free, turbulent, rectangular jet. The core of
constant velocity of such a jet was not longer than twice the diameter of
the nozzle used, At a distance of 2-6 nozzle diameters, the authors obseeri-
ed an intermediate zone between the core of the jet with constant velocity
and the main part of the jet, An analysis of the flow of a free jet shows
that the cross section of constant velocity of the jet can only be
enlarged by reducing the turbulence and energy loss in its boundary layer.
For this purpose, it is recommended to bound the jet by a solid surface.
With the aid of experimental data by other authors (D, N., Lyakhovskiy et al.,
Aerodinamika elementarnogo fakela, Soobshcheniye Tsl:TI, 1936) and on the
basis of the Prandtl equation, the following relation is obtained for the
calculation of the tangential stress of the Jet: Tc = 0 0125 Quo /2, It in
shown that the tangential stress arising with a jet flowing about a plate
is one-fourth of that of a free jet, In addition, experimental results
indicate that the lose in energy occurring in the bounlary layer of a
plate is many ti:aes smaller than in the boundary 1,-..:ter of a free jet By
Card 2/3

27243
S/17 61/004/009/002/013
Method of investigating the ... B104YB125
using a prismatic jet guide that bounds the jet on three sides, it was
possible to extend the jet core of constant velocity to a length of about
10 nozzle diameters, The width of the constant-velocity core amounted to
70j'a' of the total width of the jet guide. There are I figures and 5 refer-
ences. 3 Soviet and 2 non-Soviet.
ASSOCIATION: Politekhnicheskiy institut, g. Kiyev (Polytechnic Institute,
Kiyev)
SUBMITTED- May 15, 1961
Card 3/3

31RIDIMUM. B.
, -
Improve the work of the Office for the Promotion of Inventions.
Izabr. v SSSR 3 no.2:44 F 158. (MIRA 1113)
(Riga-Zlectria industries)

FRIDLENDER, B. 1. (Moskva)
Cruciform and T-shaped airfoils in a compreanible flow.
Inzh. zhur. 2 no.4:245-261 162. (MVU 16:1)
1 (Airfoila)

L 1553-1-63 WP(r)/WT(m)/bDS AMCIMC EM
ACCESSION NR: AP3006586 S/0020/63/151/006/1299/1302
AUTHOR: Fridlender, B. 1.
TITLE: A cruciform wingyof finite span in a compressible f ow
SOURCE: AN SSSR. Doklady*, v. 151, no. 6, 1963, 1299-1302
TOPIC TAVS: cruciform wing, wing, finite spaii wing, compressible
flow, supersonic flow, velocity potential, star shaped wing,
Chaucy problem, harmonic oscillation
ABSTRACT: Compressible flow over a.cruciform wineconsisting of
four cantilevcra of arbitrary geometrical shape is considered (see
Fig. 1 of the Encloaure).' Each of the two side cantilevers makes
arbitrary harmonic oscillation�tlibf w frequency in a supersonic
flow. The pro~ilem consists in the determination of disturbed ve-
locity potential ~(xj, y, z, t) in linear forination, which satis-
fies the equation:
2).22~ 22"1 _ a2a2 " 4 2 -22 ':Z 0- 0.
V2 - a -~j 9t2 + 2VW
3Y2 a x 13 t
Card 1

L15511-63
ACCESSION NRt AP3006586
The
An expression for velocity potential is derived. velocity po-,~
tential of the star-shaped wings with identical or different dihed-
ral angles can be determined by the same method. "The author ex-
presses his thanks to his scientific mentor Ye. A. Krasil'shchikove.".
This article was presented by Academician L. Sedov on 12 Jan 63.
Orig, art. has: 2 figures, and 8 formulas.
ASSOCIATION: none
SUBMITTED: 25Dec6Z DATE ACQ: 27Sep63 ENCL: 01
SUB CODE: Al NO REF SOV: 002 OTHER: 001
Card

ACCESSIOW VRs AP402695o
i Fridlender, Be is (Moscow)
AUMOR
TITLEs Vibraftamm at finite-opm crWif OM &jeoM IA a
cmPnesible now
SOURCE i UAIMST'1117'117 1111111AX-* # V- 4 # no - 11964 1 17-28
TOPIC TAGSt potential flow, perturbation velocity, supereonie flow, h&rmmi
vibrations, 3Amd1n,-. edge Fr*3m, airfoil, finite.spen, crucifom "rrell A
I~-:,-,;AB5MCTt The potential flow perturbation velocity over a cruoiform airfoil with
four arms of arbitrary shape is considered. Each side of the cruel f o r a . airfoil
is in supersonic flow with arbitrary harmonic vibrations of amplitude C) . The
i linear two-dimmaimal solution is given in teram of the perturbation potential,
M.NYSO ~&Vs) U (a Sit
band for the equation
+ Lev ins 0~j
I.Ccled I&

ACOWSION M: "4026950
]The Cauchy boundary probies is applied to the first oatant and Hadamard's method is,
used to present the fundamental solution in the form v - U/r. The subsonic leading,
edge problem is shown to lead- to integral equations of the,form given by To. A.
Krasillshchikova
(Kry*lo konechnogo razmakha v szhimayemom potoke. Gootekhisdatp
1952). The linearity of the problem allows one to add the effects on the velocity
from the vertical and horizontal oscillations of the airfoil. "The author
expresses his gratitude to Me sugerviack., Xe. A; MmillohdAkovae" Origo art,
b": 40 equations and 3 fle"00-
ASSOOLLTIONs none
SUBMITTED: 3OJaA63 DOR ACQs 15kpr64 ENGLe 06
SUB CODEt Al NO REr SOYs 003 TR 1 000
Q
Card 2/2
OIL I 'L i-

3402i
S/05 62/042/001/045/048
B1 54YBI 12
AUTHORS: Khulubey, Kh., Auslender, Y., Fri4lender, E~, Taitseyka, Sh.
- - ----------
TITLE: Angular distribution of p-mesons in n-p decay
PERIODICAL: Zhurnal eksperimentallnoy i teoreticheskoy fiziki, v. 42,
no. 1 , 1962, 303-304
TEXT: The anisotropy of the angular anion distribution in pion decay was
already investigated in Ref. 1 (A. 0. Vaysenbergp E~ D. Kolganoval Z. V.
Minervina. ZhETF, 41, 106, 1961). The aim of the present paper is to give
new data, of which only a few were published up to now, and to point out
that some conclusions made in Ref. 1 are unfounded from a statistical point
of view. Using the same material as for the investigation of the n-p decay
in a previous work (Ref. 3), the authors observed 1734 n-p-e decay
events and obtained the following angular distribution:
Angular interval 0 450 45 90 - 1350 1 135 - 1800
Number of i 393 412- 900 1 493 436
The forward-backward ratio b -0-143 � 0-046 indicates a deviation from
Card 1/4

34021
S/056/62/042/001/045/048
Angular distribution of B154/B112
isotropy of 2.96 of the standard errors and is therefore obtained in the
case of true symmetry with a probability of less than 3-jo-3~ The general
deviation of the observed distribution from isotropy is measured with the
probability P(,-,YZ/ - 4.6-10-3. The conditions were the same as those during
the detection of pions in T decay which was also calculated in Ref. 1.
General statistics is insufficient for determining the difference between
several partial distributions. Thus, in Refo 1, the ratio z/A is
0.958 + m61 in low-density regions (all "observers") and 0.855 � 0.052 in
high-Lnsity regions ("observers" E, F, G). This distinction of material
according to the forward-backward ratio obtained by different observers is
statistically inadmissible. The authors therefore made the following
calculation by the Monte Carlo method. From n/;r - 0-905 (corresponding
approximately to the result of all "observers" in the high-denaity region
in Ref. 1) they chose seven x-jr pairs (seven "observers") and marked those
three "observers" who had received the highest asymmetry. The volume of
the samples was approximately set equal to the number of muons in the
high-density region in Ref. 1. This was repeated ten times. For the ratio
nl.W , the following results were obtained:
Card 2/4

3!
17,
AnL;ulaz- distribution of 12
All "observers" 0.907 + OT015
Four "observers" with the lowest asymmetry 0,)62 + 0 Cl)
Difference 0.075 + O~024
Three "observers" with the highest asymmetry 0.826 + mig
There are 4 references: 1 Soviet and 3 non-Soviet. The three references
to English-language publications read as follows: Ref. 2, H Hulubei,
J. AuslAhder, B, Friedl9nderq S. TiVica. Int, Working Meeting on Cosmic
Rays, Buchurest, 1959, Acad. RPR, Inat. de Fizica Atomicd, Bucure-pti,
1960, p~ 130- J. Ausl'a'nder. Ninth Int, Ann. Conf, on High Energy Physics,
Kiev, 1959, Acad, of Science USSR end IUPAP Plenary Ses. VI-IX, Moscow,
1960, p. 239. Ref, 3. H. Bulubei, J. Aualtinder, E. Balea, E.
Fried1linder, S. Titeica, Proc, of the 2-nd Int. Conf, on the Peaceful
Uses of Atomic Energy, Geneva, 1958, P- 1283. R~ L. Garwin ot al. Phys.
Rev. 108, 1589, 1957-
ASSOCIATION: Institut atomnoy fiziki Rumynskoy akademii nauk Bukharest
(Institute of Atomic Physics of the Rumanian Academy of
Card 3/4 Sciences,Bucharest)

Angular distribution of ..,
SUBMITTED: October 10, 1961
34021
S/05 62/042/001/045/048
B154YB112
Card 4/4

1.1,40 tz)LIm. =14~p dot.-ont; FRMLIM'.`., ltz-h.
-176k~,
'1=11t-tol Of a cf problom ill t~w ,.)Y)orj
of thinctioi-P-1 intorchi.-iV. ability and prcalolw of
mchinun myl their jwts. itsm. uclliub. vav ; v=:3h4I=tr.
m.9:177-183 165. UwA is,n)

Investigation of azimuthal effects in meson showers produced b7
9 Bev protons. Zhur. eksp. i teor. fiz. 39 no.4:965-969 0 16o.
(MIRA 13:11)
1. Institut atomnoy fiziki Akademii nauk Ru;nvnnkoy Narodnoy
Reapubliki.
(mesons) (P~rotone) (Cosmic rays)

FRIEDLANDER, E.M.
Distribution of transverse impulses in meson jets at
accelerator energy. Comunicarile AR 13 no.9t8ll-815
3063.
1. Membru corespondent al Academiei R.P.R.

FRIEDLUIDER,,..~.,M.; NITU, R.
Production of high energy neutral pions in Ir- -xe collisions
at 9 BeV. Comunicar:Ue AR 13 no.9t817-820 S163.
1. Membru corespondent al Academlei R.P.R. (for Friedlarder).

FRIDLENDER, Feliks Leonidovich; TSEYTIMI, Lev Aleksandrovicb;
MARTYNOV, A.P., re-a-.-;-UMOK.HGVA, S.S., tekhn. red.
(Electronic computers] Elektronnye vycliislitellrye mashiny.
Moskva, Gos. izd-vo "Vysohaia shkola," 1961. 147 p.
(MIRA 15:2)
(Electronic calculating machines)

64-
FRIDLFIII)'.'R, G.O., and S.A. MA10ROV.
---------------------------
Membrannye aeronavigatsionno-pilotazhriye pribory. I'oskva, 190. 155
P., illus
At head of title: Krasnoznamennaia ordena Lenina Voenno-vozdushnaia
inzhenernaia akademiia in. N.E. Zhukovskogo.
Bibliography: P. 15h.
Title tr.: Membrane air navigation and nilotinE instruments.
TL589.F7
SO: AeronauticnI Sciences and Aviation in the Soviet Union, Library of
Congress, 1955

Mathematioal, Reviews 0. 0. On the precession, d #jZMMW under )7W
Vol. 14 No. 8 the action of hn external moment. A SSSR.
Sept. 1953 *"'InfenemylSbornikl2.229-233(1952). (RuWan)
Meohanics, In the usual investigations of the behavior of a gyroscope 0
under the action of nn external moment, the motion of the
axle is examined, nud the b6avior of the kinetic moment
vector and of the instantanCOU3 angulhr velocity vector are!
disregarded. The paper is concerned with the behavior ofj
these last two vectors in the case of a rap;dly retatingi
flywheel. E. Ltimanis (Vancouver, B. C.).

I J) L F_ 14 J)'C'-
PHASE I TREASURE ISLAND BIBLIOGRAPHICAL REPORT AID 325 - I
BOOK call No.: AF6o896l
Author: 'FRIDLENDER, 0. 0. and SELEZNEV, V. P.
Full Titli~. MMMTRIC INSTRUMENTS, COMPASSES AND AUTOMATIC
NAVIGATORS
Transliterated Title: Pilotazhnyye manometricheakiye pribory,
kompasy i avtoshturmany
Publishing Data
Originating Agency: None
Publishing House: State Publishing House of the Defense
Industry (Oborongiz)
Date: 1953 No. pp.: 367 No. of copies: Not given
Editorial Staff
Editor: None Tech. Ed.: None
Editor-in-Chief: None Appraiser: None
Others: Gratitude for valuable assistance expressed to:
Kozlov, A. S., Bodner, V. A., Krasovskiy, A. A.,
Chistyakov, N. I., and Bersukov, M. L.
Text Data
Coverage: This is a textbook. The author explains the theoretical
basis of each group of instruments, and shows their princi-
pal mechanisms. He mentions frequently the trademarks of
1/8

Filotazhiiyye manometricheskiye pribory, AID 325 - I
kompasy I avtoshturmany
Russian-built Instruments. Numerous diagrams, graphs,
photos, tables, etc.
This is a very good, up-to-date textbook. However the
instruments described are very similar to those built in
the USA, and nothing new In their theory and construction
has been noticed.
TABLE OF CONTENTS PAGE
Preface 3-4
Introduction 5-13
1. Purpose and classification of aviation
insturments
2. Flight with the aid of flight instruments
Flight without visibility of external landmarks
General requirements of instruments and their
errors
5. Short historical outline.
Ch. I Basic Parts of Aviation Instruments. Errors of
Instruments, and Some Methods of Compensation 14-49
1. Elastic sensitive elements
2/8

Filotazhnyye manometricheskiye pribory, AID 325 - I
kompasy i avtoshturmany PAGE
2. Methodical errors of the variometer
3. Structure of the variometer
Ch. V Magnetic Compasses 93-124
1. Some information on terrestial magnetism
2. Structure of the compass
Equation of movement of the chart
Deviation of the compass. Action of magnet
on magnetic mass
5. Equations of deviation
6. Reduction of deviation and determination of
a definitive deviation
7. Deviational instrument
8. Bank deviation
9. Deviation of higher orders
10. Turning error
Ch. VI Remote Transmissions and Indicating Systems 125-178
1. General information
2. Three-channel, potentiometric remote transmissions
3. Other potentiometric remote transmissions of
the measurer-of-current-ratio type
4/8

Pilotazhnyye manometricheskiye pribory, AID 325 - I
kompasy i avtoshturmany PAGE
Ch. VIII Remote Indicating Compasses with Inductive
Sensitive Elements 2o6-236
1. Inductive sensitive elements
2. Remote indicating inductive compass with single-
phase sensitive element
3. Remote indicating inductive compaBs with
three-phase sensitive element
4. Structure of the remote indicating inductive
compass
5. Errors of the remote indicating inductive
compass
Ch. Dc Other Features of Remote Indicating Compasses 237-247
1. Electronic remote indicating compasses
2. Generator remote indicating compasses
Magnetostrictional compass
Radio-se*micompasses and radio-compasses
Ch. X General Information on Navigation Automata 248-273
1. Mathematical problems solved with naviga-
t1on automata
2, Principal block-diagrams of navigation automata
618

Pilotazhnyye manometricheskiye pribory,
kompasy i avtoshturmany
AID 325 - I
PAGE
Speed gauges for navigation automata
Course gauges for navigation automata
Ch. XI Computing and Solving Devices in Navigation
Automats 274-307
1. Trigonometrical devices
2. Multiplying devices
Adding devices
Integrating devices
Ch. XII Diagrams of Some Navigation Automata (Automatic
Navigators) and their Errors 308-342
1. Development of navigation automats
2. Course graphs
Navigation coordinators
Errors of navigation automats connected with
the changes of altitude of the flying aircraft
Appendix Elements of Aircraft Na .vigation and Celestial
Orientation 343-362
1. Basic information
2. Elements of navigation and calculation of the
course line and of the ground speed
7/8

TIKHMKNRY, Sergey Sargey(3vich;4AII)LLUJZ.,,.,(~!~Q,,,, professor. doktor
retsenz-on't;
SALEZNW, V.P., dotsent,
tekhnicheskikh nauk,
kandidat takhnicheakikh nauk, retsenzent; HATUrM, N.K., inzhener
retsenzent; GUROV, S.Z.. redaktor; LOSKVA, G.F., izdatel'Bkijy
redaktor; ANTONYUK, P.D., tekhnichaskiy redaktor
[Alements of precision Instruments; a computation and constructicn
manual) Alementy tochnykh priborov; rukovodstvo oo reschotu i
konstruirovaniiu. Xoskva, Gos.izd-vo obor. promyshl., 1956. 360 p.
(Instruments)

PAVWV, VsA., imndidat takhm4olkeskikh nauk, detment; TUNIMANOV, A.Z., inzbomr;
A~P~Yt A.K., insbener; GUSHCHIRL. L.M.. inzbener; RIVKIN, S.S.,
dolctor tokhaicheskikh neuk; SAYDOT, P.I., kandidat t*khnicbesklkh nauk
dotseat; PZLIPOR. D.S.. doktor tekhnicheskikh nauk, profewwr; XWOV.
B.L.. Aoktor takhnicheekikh nauk, professor; TIKHMMT, S.S.. dolctor
takhiiicheskilch nauk. professor; PRIDUNDIR. G.0.. doktor tekhnicheskikh
naui. professor: CHISTYAXOT, N..L., aOO'k T�rlMnichaskikb nauk,.profes-
s0r,
di~m T.A. kavlov's book -Aircraft gyroscope instrumentsm be recommeuded
tor use an a textbookW Priborostroade no.h.29-31 Ja 157.
M" 10:4)
1. Ghlen praylenlys Leningradekogo otdoloniya nauchnogo iuahenerno-
tekhnicheskogo obahchestva priborostroitellnoy promyshlennostl (for
TunimanoT). Chlen praylonlya Vessoyuznogo nauchnogo ij=henerno-
takh.nichaskogo oblah.chastva priboroetzoitel'noy prou7shlonnosti (140r
Gushchina) 30toskovoikoye Tyasheye takhnichaskoye Uchillshche imeni
AkWom (for )Fellp9r, Tikhmenev). 4. Hookovskiy aviatsionnyy institut
imeni Serge Ordshonikidse (for-Wabov). 5. Voyanno-vozdushnaVa in-
zhenernays, akademlya imeni N.Te. Zhukovskogo (for Chletykar)
(Gyroscope)

/,Z)
i
SWMTANSKIT, Grigorly Aleksandrovich; PAYADILOV, Yuriy Nikolayevich;
-FRIDLXMNt, G*Oo, prof., doktor tekhn. nauk, retsenzent;
inzh., red.; PMOTA, I~A*, red. Isd-va;
PUMUJKOVA,, NA90 tekhn, red,
[Floating g7roscopsis and their use] Poplavkovys giroskopy I Ikh
primenente. Koskm, Goo. izd-vo obor. promyshl., 1958. 243 p;
(Gyroscope) (AIRA lIt8)

69936
S/024/59/000/06/013/028
E031/E213
AUTHOR~' Fridlender G. 0" (Moscow)
~- - I - -
TITLE; A System for Determining the Parameters of Motion for a
Body in Space \V
PERIODICAL. Izvestiya Akademii. nauk SSSR, Otdeleniye
tekhnicheskikh nauk, Energetika i avtomatika, 1959,
Nr 6, PP 108-117 (USSR)
ABSTRAM, The body is assumed to be in a weightless state in inter-.
planetary space. The author considers a scheme which
makes use of the properties of a system corrected from
the second integral of the measured accelerations. Tile
system consists of three gyroscopes~which are at rest
relative to the stars. Ir the quality of the gyroscopes
is insufficiently good, the immobility of the system can
be guaranteed by two optical systems directed on any two
stars. With the gyrosystem are connected two platforms
each of which has two degrees of freedom with respect to
the gyrosystem, The two angles of inclination of the
first platform with respect to the gyrosystem are assumed
proportional to the repeated integral of the accelerations
measured in two mutually perpendicular directions by
Card 1/5 accelerometers on the first platform, The repeated 1"k

69936
S/024/59/000/06/013/028
E031/E213
A System for Determining the Parameters of Motion for a Body in Space
integral of the acceleration', measured by the third
accelerometer on the second platform, determines the
position of the second platform. Thus the repeated
integrals give the path in interplanetary space, and the
simple integrals give the velocity, under the assumptions
that the effect of the acceleration due to the gravitational
fields of the Sun and the planets, as well as the instru-
mental errors of the system,., can be neglected. To eliminate
the errors the following set-up can be used, It is
supposed that there are two optical systems directed on
two planets or the Sun and a planet. The angles of
inclination of the first platform must be proportional to
the sum of the repeated integrals of the accelerations
and of the angles of inclination of the platform with
respect to the first optical system. The position of the
second platform can be determined by the repeated integrals
of the accelerations and angles with respect to the second
optical system, An example is considered of a spherical
system of coordinates whose reference plane coincides
Card 2/5 with the plane of the ecliptic and whose reference meridian

09936
S/024/59/000/06/013/028
E031/E213
A Svsttim~ for Determining the Parameters of Motion for a Body in Space
passes-through the point of the vernal equinox, The
radius vector r makes an angle 0 with the refererce
plane and the azimuthal angle is denoted by a. The
first platform is perpendicular to the radius vector, so
that its angles of inclination wi.th respect to the
gyrosystem are 0 and a., Correspondingly, the angles
of inclination of the radius vector ZNO and P defined
by the first optical. system must lie in the meridian
plane and in the plane perpendicular to it through the
origin,, The second platform is oriented so that the axis
of measurement of the third accelerometer coincides with
the direction of the radius vector, The system desc-~-ibed
above has the disadvantage that four optical systems
are required, but the advantage that the velocity error
can be made smaller than in systems where the velocity is
obtained by straight differentiation. The equations of
motion of the platform are now considered. Expressions
are derived for Z_%O, 0 and the angle of
inclination of the second platform with respect to the
radius vector, If /",.0. 0 and Z-, t~ vary not only
Card proportionally to the repeated integrals of the

69936
S/024/59/000/06/013/028
E031/E213
A System for Determining the Parameters of Motion for a Body in Space
accelerations but also proportionally to the slims of the
repeated and single integrals of the angles themselves,
additional terms appear in the expressions, The second
order differential equations of motion are derived
from these extended expressions., The period of
oscillation of the platform and the values of the
coefficients in the equations are determined from the
required accuracy of the velocity readings. The stability
of compensation for the systematic errors is discussed.
General conclusions of the paper are-. 1) The use of
a gyrosystem. for motion in interplanetary space is
complicated due to the "weightlessness" of the sensitive
elements of the accelerometers and the consequent absence
of a correction created by a period of no disturbances;
2) The method of repeated integration of the discrepancy
between the calculated and the true readings avoids the
above difficulty and makes possible the determination
of the parameters of the motion in space; 3) The method
Card 4/5 makes it possible to obtain a period of the system IIK

69936
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E03l/E213
A System for Determining the Parameters of Motion for a Body iii Space
significantly less than the period of no disturbances and
to introduce damping without the system being disturbed
by accelerations. There are 4 figures and 2 references,
1 of which is Soviet and 1 English.,
SUBMITTED.-. October 15, 1959
Card 5/5

_:37
PHASE I BOOK EXPLOITATION SOV/4364
Bodnerp Vasiliy Afanaslyevich, Gavriil Oskarovich Fridlender, and Nikola7
Iosifovich Chistyakov
Aviatsionnyye pribory (Aircraft Instruments) Moscow, Oborongiz, 1960. 512 p.
Errata slip inserted. 10,000 copies printed.
Reviewer: B.A. Ryabov, Doctor of Technical Sciences, Professor; Ed * (Title page):
V.A. Bodner, Doctor of Technical Sciences, Professor; Ed. (Inside book):
O.N. Burakova; Tech. Ed.t L.A. Garnukhina; Managing Ed.t S.D. Krasillnikov,
Engineer.
PURPOSEs This is a textbook for students of aviation institutions of higher edu-
cation taking a course on aircra-ft instruments. It may also be useful to en-
gineering and technical workers Interested in instrument production.
COVERAGE: The book presents the theory, construction principles, specicl features,
operating principleap and design elements of instruments controlling power plants
and piloting and navigating instruments. Special attention is given to the
theory of errors and methods of instrument compensation. The book also discusses
measuring methods and diagrams of instruments which may be used In the future.
The introduction and Chs. Is III, Vs VIO VIII-XIV, see. 1 and 2 of Ch. IV9
C"d-1/.9"

A.ircraft Instruments SOV/4364
and sec. 1. 2, 3, 5 of Ch. VII were written by V.A. Bodner; Ch. II, see. 4
of Ch. V'II, Sec- 1-4 of Ch. IV, see. 1-6 of Ch. M and Ch. IVII by G.O.
Fridlender; see. 3-5 of Ch. IV by N.I. Chistyakov; sec. 5 of Ch. XV, and
see. 7 of Ch. XVI I by M.S. Kozlov; parts of sec. 5 of Ch. XI, and sec. 5 of
Ch. X11, by V.V. Olizarov. No personalities are mentioned. There are 31
references, all Soviet.
TABLE OF CONTENTSt
Foreword 3
Introduction 4
Ch. I. Electrical Methods of Measuring Nonelectrical Quantities 9
1. General information 9
Parametric Measuring Methods
2. Resistive method
3. gapacitive method
4. Inductive method
5. Magnetostrictive method
Card 2/9
11
11
17
23
29

80951
s/o24/60/000/03/013/028
-3,3000 E140/E463
AUTHOR: Fridlenderg G.O. (Moscow)
TITLE: On the VanishTrig-of Limited Damping in Inertial
Systems Operating in the Indicator Regime During
"Fugoidal" Flight*
FERIODICALz Izvestiya Akademii nauk SSSR, Otdeleniye tekhnicheskikh
nauk, Energetika i avtomatika, 1960,j Nr 3, pp 106-11OWSSR)
ABSTRACT: In inertial systems according to Leventhal consisting of
a &X:~over,~i~cal~ corrected by moments proportional to
the integral of the accelerometer9output signal, damping
may be realized by applying to the gyroscope an additional
moment proportional directly to the accelerometer signals
ie by-passing the first integrator by a direct coupling.
Analysis shows that the introduction of damping gives rise
to a perturbation during changes of acceleration. Both
Leventhal (Ref 1) and the present author have proposed
limited damping to reduce this factor. It is demonstrated
in the present article that with fugoidal flight the
effectiveness of damping is sharply reduced to the point
where it may be considered as absent. To restore damping,
Card 1/2 it -Js necessary to have additional information on

0951
S/024/6o/ooo)03/013/028
E140/E463
On the Vanishing of Limited Damping in Inertial Systems Operating in
the Indicator Regime During "Fugoidal" Flight
acceleration which may be subtracted from the
accelerometer output. Two such sources are Doppler-
effect information and aerometric. information, both of
which must be differentiated to obtain acceleration.
The simultaneous use of limited damping and accelerometer
correction by differentiated aerometric velocity
measurements can make an inertial system damped and
extremely stable. There are 3 figures and 2 references,
I of which is Soviet and 1 English in Russian translation.
SUIUMITTED: December 18, 1959
*[Annotation: "Fugoidalm should be "Phugoidal" throughout the
article]
Card 2/2

F~IDLIZI)ER,-CI.4yr;LII-Qska~~-qyiqhi~OBOIEV, O.K., red.; AKSELIROD, I.Slt.p
tekhn. red.
(Inertial systems of navigation] Inertsiallaye siatenq navigateii.
Moskva, Gos. izd-vo fiziko-matem. lit-ry, 1961. 153 P.
(MIU 24: 11)
(Inertial navigation (Aeronautics))

t, -
PHASE I BOOK EXPLOITATION SOV/5933
Fridlender, Gavriil Oskarovich, and Mikhail Stepanovich Kozlov
Aviatsionnyye giroskopicheskiye pribory (Aircraft Gyroscopic
Instruments) Moscow, Oborongiz, 1961. 390 P. 15,000 copies
printed.
Ed. (Title page): V. A. Bodner, Doctor of Technical Sciencess
Professor; Reviewers: B. A. Ryabov, Doctor of Technical
Scienceep Professorp and P. V. Bromberg, Doctor of Technical
Sciencesp Professor; Ed.'of Publishing House: I. A. Suvorova;
Tech. Fd.: A. Ya. Novik; Managing Ed.: S. D. Krasiltnikov,
Engineer.
PURPOSE: This book is intended for advanced students concerned
with aircraft aid dreraft Instruments. It may also be useful to
engineers in the aircraft and instrument industries.
COVERAGE: Theoretical fundamentals and design and structural
features of modern aircraft and -ocket gyroscopic Instruments
Card 1/1

Aircraft Gyroscopic Instruments
SOV/5933
curLe)tly in use are given. Principles employed in the design
oi precision gyroscopic systems such as inertial vertical gyros,
floating integrating and rate gyros, and gyroscopic instruments
with integrating correctionsare discussed. In the theoretical
discussion of the instruments, special attention is given to
dynamic properties and errors. Calculation methods, numerical
examplesp and descriptions are given for many instruments.
No personalities are mentioned. Chs. Ip III, IV, and VIII were
written by G. 0. Fridlender, and Chs. II, V, VI, and VITs by
M. S. Kozlov. There are 16 references, all Soviet.
TABLE OF CONTENTS:
Foreword
Ch. I. Fundamentals of Gyroscopic Theory
1. General information
2. Coriolis acceleration
3. Gyroscopic precession
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3
5
5
6
9

GORNSHTEYH, I.A.; SHULIMAN, I.A.; SAKEYAN, A.S.; FRIDLENDER, G.O.,
prof., red.; VOLKOVA, I.M., red.; BEIYAYEVA, V.V., tekbr. red.
[Inertial navigation]Inertsiallnaia navigatsiia. Pod red. G.0.
Fridlendera. Moskva, Izd-vo "Sovetskoe radio," 1962. 248 p.
(MIRA 15:12)
(Inertial navigation)

ANDREYEVA2 L.Ye.,,- FEDDOSIYEV, V.I.., doktor tekhn. nauk., prof.., red.;
--JMDLWER-,-Gv4,p doktor tekhn.naukv retsenzent,- AKIMVA,
A.G.j. red. izd-va; ELIKIND, V.D., tekhn. red.
(Elastic elements of instruments]Uprugie elementy prilx)rov. Pod
red. V.I.Foodooleva. Moskvap Mashgiz, 1962. 254 (PM31?A 15:9)
(Yeasuring instruments)

VENGEROV, V.A.; DEMIDOV, I.S.; FRIDLENDER. G.0.
Precision balancing and the determination of w~even rigidity
of elastic mechanical.aystems. Ism. tekh. no.1000-32 0 163.
(MIRA 16:12)

DANILIN, Vasiliy Petrovich; TlKfll-'~IIEV, S.S., zasl. deyatell nauki
i tekhniki, doktor tekhn. nauk, retsenzent [deceased);
MAKSIMOV, V.V., dots.) ret8enzent; ARUMEOV, S.S., dot.s.,
rotsonzent; FRI-D'WIDER, G.O., prof.0 nauchn. red.;
TITOVA, V.A., red.; DMULOVA, V.V.., red.
[Gyroscopic instruments] Gli-oskopicheskie prJbory. Moskva,
Vysshaia shkola, 1965. 538 P. (MA 18:t)

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ACCEtSIC0 Nk.____Ak6_0_15'522_ UR/0286/651000/006/0058/0058~
620.178
AUTHOR: Ganin G. 0.; Chachikyan, R. G.
V. P.; Opukhovskiy, rridlender,
JITLE: A unit for checking and testina automatic catapulting devices. Class, 42,
Y__
~No. 170184
!SOURCE: Byulleten' izobre*teniy i tovarnykh znakov, no. 8, 1965, 58
!TOPIC TAGS: catapult, test equipment
;'ABSTRACT: This Author's Certificate introduces: 1. A unit for checking and test-
atapulting devices. The mechanism contains a frame with a sleeve
'ing automatic c
.which is placed on a rigidly fastened axle turned by a motor. The eevice is de-
signed for simulating catapulting..Ioads which are close approximati2cns of actual
Iloads. Fastened to the frame are two guides which are joined through a system of
.three interconnected sleeves to a shaft whict. is rotated and moved along these
guides by_a crankshaft connecting rod mechanism. On one end of the shaft is a
.table for the devices being tes~ted, and on.the other end is a sprocket which is con
Inected by a chain drive to another spr4~cket rigidly fastened to the base of the
Card 1/3

L 51435-6j_
IACCESSION R:_ ~&~015522
,unit. 2. A modification of this installation which uses a system of four levers
jor keeping constant tension on the chain drive when the shaft is being moved
~along the* frame in a radial direction. Two of these levers have one end swivel
;connected.to the table shaft, while the other two have one end connected in the samJ
way to the sleeves of the frame. . The other ends of the levers are ccnnected - in
ipalra to intermediate axles with sprockets rigidly connected to them. 3. A modifi-1,
Cation of this -installation which contains a balancing unit made up c,.f a weight
located on a guide frame symmetric with the table shaft and connected, with the
shaft sleeve through two swivel-connected levers-and a rocker.
77 4330CIATION: -Organizatsiya~ go-skovifteta-po aviatsionnoy tekhnike SGSR (Organization I
04-- t'he State Committee for Aviation Tochnol Lgy,_q~~R)
GUB COM; IE
-qUBHITTED: S 0
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NO REF SOVv 000 OTHEM 000
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ACC NRi AP6002160 AST/GW/BC, SOURCE CODE: UR OOb7_0O_P0_16_0/T1W'
AUTHOR:./Fridlender, O./(Moscow; Deceased); lof - T. (Moscow)
ORG: none
TITLE: A method for determining the parameters of motion% a,nd orientation of an
object in the vicinity of a planet
SOURCE: AN SSSR. Izvestiya. Tekhnicheskaya kibernetika, no. 6, 1965, 160-166
TOPIC TAGS: astronautics, autonomous navigation system, attitudo control
ABSTRACT: Difficulties arising.~n determining the flight and orientation parameters
of a spacecraft flying in the vicinity of a planet of the solar system and controlled
by means of autonomous navigation systems utilized in aircraft and spacecraft are
indicated. An autonomous navigation system consisting of an optical indicator for
determining the local vertical, the gyrosystem, three accelerometers, and a
computing unit for space flights in the vicinity of a planet is proposed. General
equations of motion of the controlled spacecraft in three-dimensional space, with the
altitude and the angle of the orbit with the equatorial plane taken as variable, are
derived. It is deduced from this that the proposed navigation system makes it
possible to determine the parameters of motion of the center of mass and the orienta-
tion of a controlled spacecraft around its center of mass during maneuvers and
free motion in a gravitational field. Orig. art. has: 2 figures and 12 formulas.[LK)

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Chemistry - Aluminum, Films of
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Electrolytic Aluyain=41 B. V. Deryagin, P. M.
Fridlyand, Inat of Phys Chem, Acad Sci UWE, 6 pp
I'Zhur Tekh Fiz" Vol XVIII, No 11 - t -1 *45- 4Y
Measures by optic methods thickness of an oxide
film on aluminum for various intensities of
oxidation. Results of measurements showed that
at any rate In the limits of 5-170 V, ox1aa9ion
occurs for fixed gradient equal to 8.5 x 10
V/cm, of potential on the film. Submitted 7 Apr 4a
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from different inetals. Izv. 1~1 hIT no.2","I-31 ( m 1!-, ,~ I F, : -) 1,

SENA, L.A.; FROLYAND, R-H. .
Formation of the cathode spot on the mercury-dielectric boundary
in ionized gas. Zhur.takh.fis. 29 no-1:3-11 Ja 159.
(HIRA
1. Nauchno-Issledovatellakly institut postoyannogo toka
(Cathodes) (Electric discharges through gaseel
12:4)
Leningrad.

SENA, L.A.; nPLTqD, R.M.
Conditions leading to the origination of inverse firing due to
mercury drops. Izv.NIIPT no.907-45 162. (MIM l5sl2)
(Mercury-are rectifiers)

aspl r:tnt.
Th(~,nry of h,3~if. conditi, ns an-A lt.1 a:~f,llcp.'Aon in tie
cs1cii1atior. oi Nh.'i teairfiratilr-3 I'Lolds A'.,- ril.-
Nfrich. trutiy Y"'i-11: no.2' 42K-18? 164.
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AID P - 4210
Subject USSR/Engineering
Card 1/1 Pub. 103 - 11/20
Author : Fridlender, I. G.
Title Determination of Rigidity In Machine Tools
Periodical : Stan. I instr., 1, 33, Ja 1956
Abstract : The author presents a simple method for determination
of rigidity (by inaertion of the indicator between the
tool-block and the machined piece) and provides for-
mulse for practical calculation of rigidity In the
line: body of machine, cutting tool, machined piece
and machine-tool attachments. Two formulae and one
sketch.
Institution None
Submitted No date