SCIENTIFIC ABSTRACT VINOGRADOV, P.A. - VINOGRADOV, R.I.

• Document Type: CREST
• Collection: Scientific Abstracts
• Document Number (FOIA) /ESDN (CREST): CIA-RDP86-00513R001859920007-0
• Release Decision: RIF
• Original Classification: S
• Document Page Count: 100
• Document Creation Date: November 2, 2016
• Document Release Date: September 1, 2001
• Sequence Number: 7
• Publication Date: December 31, 1967
• Content Type: SCIENTIFIC ABSTRACT

-L ~5461-63 EPR/EWP(J)/EPF(C)/ZW(M)/BDS AFFTCAsD Pi-4/Pc-4/pr-L
PM/WW
ACCESSION NR: AP3005443 3/0020/63/151/005/1118/1119
AUTHORS: Turov , B dov P. A,.; DolSop1osk,,. B. A. (Corr.
Member AS, SSSR); 44- A. W-Wo 1 7
T17LE: Influence of olootron donor additives on the chain
structure in stereospecific polymerization of butadiene
SOURCE: AN SSSR. Doklady, v, 151, no. 5. 19'3p 1118-1119'
6
IOPIC TAGS: electron donor , butadiene polymerization,$ stereospoeific
olymerizations cis-polybutadiene,,trans-polybutadiene
.p
ABSTRACT: The affect of thio-others and tertiary amines (dibutyl
sulfide and triethylamine) on butadiene polymerization was studied-as i
a continuation of earlier study by the authors (DAN, 1469 1141 (1962))!
of the effect of straight others, These compounds had less effect
on polymerization rate than the straight ethers. They did affect an
increase in thejamount of 1.4-trans isomer by decreasing the LA-cis-
polybutadign&,,~qThera was no lowering of solubility or uneaturation ln~
the polymer formed. Experiment shows the cis-polybutadiene does not
Card 1/2

L 15461-63
ACCESSION NR: AP3005443
undergo changes in presence of donor additives and components of the
catalyst system TiI)~ + (iso-ChHq)-AA1 Trans-meafbers are fbrmd only in!
tEe polymerization process by tria-cu act participation of complexes
containing the electron-donor additives. Orig. art. has: 1 figure. i
ASSOGZkTION*, Yarovslavakiy zavod sintatichaskogo kauchuka
(Y synthatic rubber plant)
,P;!0SlaV
SUBMITTED: 07MaY63 DATE ACQ: 06Sep63 ENCL: 00
SUB CODE: M, CH NO REP SOV: 003 07HER: 003
~~Card 2/2
V
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51 T -A Z~N 4

TUROV, B.S.; vrNCGRADOV,P.j',.; DOLGOPIC-SK, B.A.; KOSTRIA, S.I.; KAS!I--,F.SKI7,
LOS
Effect of electron-donating additlonB on the chain wicroarructurf)
in 'he st. ospecific polymerization of butadiene in the presence
of "cobal-11 catalytic systems. DokI. AN SSSR 155 no. 4:874-875
Ap 164. (MliA 17-5)
1. Chlen-korrespondent AN SSSR (for Dolgoplosk).

VW-rl I kworA I
Ap6ooo986
Gavehinovat Ke Yee
ORGi none
TITLE: A method for obtaining synthetic rubbe Class 399 12. IJ6410 rannounced by
Yaroslavl Technological Insti -f-c-oslavskiy tekhnologicheskly instilutY
tu, 0 Yar
SOURCE: Byulleten' izobreteniy i tovarnykh znakovq no. 229 1965, 6o
TOPIC TAGS: polymerp polymerization, copolymerization, synthetic rubber, rubber
ABSTRACT: This Author Certifigate presents a method for obtaining synthetic rubber by
low-temperature Polymerization'Pof dienes or copolymerization of the batter with vinyl
monomers in an aqueous emillsion in the presence of redox initiatora.N To obtain
modified rubbers, the polymerization or copolymerization process is carried out in the
presence of 8-chloretbyl ester of metbacrylic acid,
MM CODE t 11/ SM DATE: 10jul.63
SOURCE CODEt UR/0286/65/000/022/0060/00601
AUTHORSi Mironovap N. M.; Farberovp Me I.; Vinogradovp P. A 7AUdwav, N. D ;
card

VrNOGRADOV, P.B.
Coments on G.r.Tollfsonte artiele *Roman Sergeerich Chatyrkin.1
Gig. i Ban. n0-11:51-52 N 154. (MIRA 7:12)
jiglyany I Loningradekogo meditsinskogo
1. Is lafedry obsbobey
Institut& iment akademika I.F.Parlova.
(BlOOPAPH13S,
Chetyrkin, Roman Sergeevich)
(MBDICM, XMITARY AND NAVAL, history
oontribution of Chatyrkin, Roman Sergeevich)

VINOGRADOV. P. B.
"Studies on the history of the public health system in Magadan Province"
by A.F Khoroshev, Reviewed by P.B.Vinogradav. Sov.zdrav. 20 no.1:
81-82 161. (MIRA 14:~)
(MAGADAN PROVINCE-PUBLIC HULTH) (KHOROSHEV, A.F.

TINOGRADOV, P.D.
- :I
H;alth problems in N.I. Pirogov's works. Trach. delo no..3:321
Mr '57 (NIaA 10:5)
1. Wedra obahchey giglyany (zav.-prof. I.Ye. Ramm) Pervogo
Loningradakogo meditainskogo instituta.
(PIROGOV, NIKOLAI IVANOVICH, 1810-1881)

VINOGRADOV, P.D.
Geology of the Zeravehan-Gisoar &ntimony-rwrcury belt. Inform.-
sbor.VSEGEI no.46:17-35 161. OURA 15:3)
(Tien Shan-Antimony) (Tien Shan-Marcury)

MARTYSHXV, V.R.; MISVIKOV. Tu.X.; TORSHIN. M.S.
Manifestations of petroleum In Silurian deposits of central Tajiki-
stan. Hat. VSEGBI no.10:73-78 156. (MLRA 10:1)
(TaJIkistan-Petroleum geology)

Name: VINOGRADOV, F. I -
Dissertation: Biological principles involved in producing early bIgh
yields of tomatoes in Moldavia
Degree: Doc Biol Sci
Min Higher Education USSR, All-UnioD Order of Lenin Acad
of Agriculture imeni V. 1. Lenin, Inst of Genetics of Acad
Sci USSR
Place: 1956, Kishinev
Source: Knizhnaya LetopiBl., No 4, 1957

L 6387~=65 E*;iT(1)/EliT(m)/r-;,F(r-)/ii~F(n)-2/i;,Ij(rn~/E,,A(d)/~'~'iP(t)/E';Ii,(k
ACCESSION NRi AP5015082 UR/0114/65/000/006/0022/'C'024
0 1 '_1 536.24-001-5
AUTHOR: Puchkov, P. I:
~Candidate of technical sciencesh
Vinogradov, 0 - i2gineer)
:2L
f-1-- -.T
TITLE: Longitudinally f inned_h~-tr~jffl surfaces
SOURCE: Energomashinostroyeiiiye, no. 6, 1965, 22-24
TOPIC TAGS: heat transfer, finned tubing
ABSTRACT: The results are reported of an experimental Investigation of the heat
,transfer and hydraulic resistance of two 1-m long 32-mm OD iret-,-. tubes; one tube
was equipped with 12 and t?ie other with 28 longitudinal 11-inm ilgh fins. Tne tubes
,2
had an inside electric I.eater, and were ccoled by air, at. 105-5x1()r' n/r, , in a
iclosed-type ga3odynaaic outfit. Critical functi-C)no Nu = f'kR-j -ind ~ . f(Re) are
presented In the form of' curves. To enhanca the heat transfer, the adr between the
fins, In the 26-fin tube, was turbulized bY 3 ring diaphragms cutting through the
I
!fins. Also roughening the fin surface was tested as a measure to improve ~he heat
transfer. Longitudinal finning Improves ny a factor of 2.4-2.7 the energ:y
i characteristics of a smcoth tubel the dlaptiragms and rough 3uface make them still
lbetter (by 7% and 20%,respectively). Orig. art. has.- 5 figures, 8 formulas, and
I table.

L 6381
Card 2/2,
ENCL.- 00 SUB ZODE: PR
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Ok

PUCHKOV, P.J., inzh.; VINOGRADOV, O.S., inzh.
Study of heat exchange and hydraulic resistance of helical channels
with heat emitting internaLl- surface. Teploanergetika 11 no.10;
62--65 o 64. (MMA 18:3)
1. TSentrallnyy kotloturbinnyy Institut.

L 64482-65 -1 0r; P (. C n t T, '~j,
ACCESSION 14'R: AP5021230 UR/002 0/65 /163 /00 5 /1"7 /1150
AUTHOM: Vinogradov, P.-A.; Dol~o )Iosk, B. A. (Academician); ZgonniJ,, V. 1J.;
ParenaF,q, 0. P.- TiT&TI-ovr, Ye. I.; ~Urovj fl.
TITLE: The role of electron--donor addiLives, watt-r, and alk-,Latinv arnntr, .7-, the
ymerization of butadiene under the influence of a cobal'-
stereorspecific pal
catalytic system
SOURCE: AV SSSR. Doklady, v, 163, no. 5, 1965, U47-1150
TOPIC TAGS: stereosp cific po r I z a Uon , I--- -"y=-er , but. iee n-- , cc ba t 0 c a t - 1~ at
lymw
ABSTRACT: The object of the investigation was to enlarge the currently available
Information concerning the stereospecific catalytic activity of cobalt cataly-tic
systems (B. S. Turov and P. A. Vinot-radov i dr., D,0, 155, 874, 1965). -he
polymer studied was butadiene. The e7perimental r,3sults are shourn -,raphically ir,
Figs. 1 and 2 on the Enclosure. It is Concluded that tbe addition ~f AICI 39
RAIGI , Br2, H20, CH = CH - CH ha-lo-on, PC1 - A-1 - 0 - A.1 - RC1 increascs the
2 2 2
formation of 1.4 cis rings, the molecular weight, and the rate of polymerization,
whereas the addition of R Al. RSR, ROR, R-Np KC1, and NaCl decreases the number
3
Card 1A

f -L 64482-65
ACCESSION NR: AP50212-90
of lp2 rings, the molecular weight, and the rate of polymerization. Orig. art.
has: 1 tablet 3 graphs, and 3 equations.
ASSOCIATION- Listitut neftekhmichoskogo sinteza, Akademii nauk, SSSR (Institute
for Petrochemical Synthesis,kadca of Sciences SSSR)
4
SUB14IMD: 151br65 ENCL 1 02 SUB CODE: DC
NO REF SOV, 007 OTHER: 005
Card 2A

L 64482--65
ACGMSION NR: AP3021280 ENG14SURE, 01
0
wu t4
0
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L
loc.,
0
'w'u0
rj
"k lio-V
1: rot,
Fig. 1, The effect of triisobutylalum'inu"m'on the number of !j2 rings in
the chain (-I), yield of pol,=er (2), and characteriatic vincosity
(3). Concentration of CoC12 = O.ON6 m mole, Al/co = 150:1
(mole), ~-)utadieno 12~-.5 9, concentration of butadiene Ir, benzer'3
1.8 mole/liter, tenperature of polymerization 30G, duration of
Card 3A experiment 20 hours.

.L 64482-65
ACCESSION PM AP5021280 ENCLOSURE: 02-
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K
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0
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?J-vo
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147 cD
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k1ple rat;a
ALUC&Hj)'Cl.
1. 1 - -1
Fig. 2. Effect of KC1 and NaC1 on the number of 1,2 rings in the chain
(1, 11), viscosity (2, 21) pol, Id (3, PI - for KU 1 2 3
,m.ar yle 9 p
for NaCl 11, 21, P. Concentratinn nf CoCl') 0.00% m mole, AI/Co
I
150:1 (w19), butadlene 12.5 g, concentration of butadiene in
benzene 1.8 mola/11~ar, Iemporaturr- of polymerization 56C, dura-
tion of experizent 1A, houre.
Card 4/4
MENEM=
9 j W~12NIA Ot QWN24wi-61

VMICGRADOV, p. I., Doc Biol Sci (disa) -- "The biological principles of obtain-
ing earlier and larger harvests of tomatoes In Moldavia". Makhachkala, 1959.
43 PP (Min Agric Ulcr SM, Ukr Aced Agric Sci), 180 copier, (KL, 71o 24, 19592 131)

VINOGRADOV, F.I., kaud.ee1'skokhozyaystvennVkh nauk
Developing cold resistant early tomato varieties In Koldavia,
Agrobiologiia noo 3:336-360' YW-Je 160. (MIU 13 t12)
(KolUvia-Texato breeding)

1. VIVOGRADOV) r. I.
2. =R-4600)
4. Tomatoes
7. Imnroving tomatooes by intravarietal crossing. Sel. i sem. Eo- 11, 1952.
9. Monthly List of Russian Accessions, Library of Congress, February 1953. Unclassifted.1

36-58-9/12
AUMOR: Vinogradoy, P. L.
TrM: The Electrical Potential Gradient in the Atmosphere Based an
Observations at Zuya, 1943-1950 (Gradiyent elektricheskogo potentsials. -ir
atmosfere po nablyudenirm v Zu-ye za 1943-1950 99.)
PER10DICAL- Trudy Glavnoy geofizicheskoy observatorilp 1956, Hr 58, PP 58-68(ussR)
ABSTRACT: Observations were conducted at the ZWa Magnetic ObserNstory vith,.a
Benndorf-type mechanical electrograph. The author discusses various points
of practical application in the findings obtained and arrives at the conclusion
that yearly variations In the gradient are expressed by a curve witli a simple
maxim= for February (162 v/m) and a flat minim= for mmmer (94 v/m). The
rate of change is in inverse ratio to the average value of the turbidity
factor. The cia-ve of daily changes was found to have two maximums and two
mi-ni7mim . There are 3 figures, 3 talbles, and 9 references of vhi.~h 8 are
Soviet and 1 English.
AVAILAME: Library of Congress
Card 1/1

VINOGRADOV, P.L.
Observations In U7 during 1943-1950 on the alectrc potential
gradient In the atmosphere. tnAr GGO no.58:58-68 056,
(MLRA 10:1)
(ZW-Atmospheric electricity)

Ir-McGloov, P. L.
2. USSR
he- Mloldavia p Tomatoes
T, P:Lanting tomatoes early in April in Moldavias Dost selikhoz. no. 1,, 1952.
9. Monthly List of Russian Accessions, Library of Congress, January, _1953. Unclassified

30125
S/194161/000/007/042/079
27 . Ll 00() D201/D305
AUTHORS: Tabarovskiy, I.K., Gofman, 1.11.,-Vinograrloir, P -H
Pushkarev, A.A. and Pomelltsov, A.11.
TITLE: An electro-kymograph, scintillation model 3KC -60
(EKS-60)
PERIODICAL: Referativnyy zhurnal. Avtomatika i radioelektronika,
'no. 7. 1961, abstract 7 E15 (Novosti med. tekhn.,
1960, no. 5, 41-63).
TEXT: The graphical recording of pulsating movements of the car-
diac vessel cluster as observed using X-rays e1. kymography, is used
for diagnosing not only cardial vessels but also pulmonary diseases,
e.g. cancer. The model EKS-60 has been approved for series induc-
tion. It permits simultaneous registration of the elctro-cardio-
gram and of one of the following processes: The pulsation of heart
periphery and of large blood vessels, the capillary pulse of the,
pulmonary parenchyma, diff. pulmonary ventilation. It is also pos-
Card 1/2

An electro-kymograph...
0125
3/1194
,/61/000/007/042/079
D201/D305
sible to register simultaneously the diff. pulmonary ventilation of
both lungs or of any 2 electrocardiogram connectors. Either a stat-
ic or scintillation slot diaphragm probe is used. The probe oscil-
lations are applied simultaneously after amplification to a recorder
and an oscilloscope. Provision is made for signalling in case the
probes and indicators are located separately. The construction is
given of the probe together i-rith the diagr&a of a 2-channel balanced
photo amplifier with noise compensation circuits and of a 2-channel
oscilloscope and of power supplies. The recording channels from
the scintillation and static probes have a frequency band 0.15 to
12 c/s and 0.04 to 8 c/s respectively. The horizontal oscilloscope
sweep is regulated from 0.01 to 10.0 sec. The overall equipment
power consumption is 1 kVA. Results of clinical experiments are
given. 29 references. Z-~bstracter's note: Complete translation.2
Card 2/2

3/028/.60/000/011/006/00-1
B020/BO58
AUTHOR: Vinogradov, P. M.
TITLE: Diamond Wire-drawing Dies rocl 6271-6o (GOST 6271-60)~ Valid
as From January 1, 1961 \A
PERIODICAL: Standartizatsiya, 1960, No. 11, pp. 36-39
TEXT: The new standard provides for the following four types of diamond
wire-drawing dies for the drawing of wires\1with a diameter from 0.03 mm
and less up to 1.2 mm: 1) UM - for the cold-drawing of very soft metals
and alloys with a strength of less than 20 kg/mm2 (Al, Zn, and others);
2) M - for the cold-drawing of soft metals and alloys with a strength
from 20 to 50 kg/MM2 (Cu, Ag, Au, Pt, and others); 3) P - for ;he cold- 2
drawing of semihard metals and alloys with a strength from 50 to 100 kgb~
(brass, bronze, Ni, Constantan, Manganin, and others); and 4) T - for the
cold-drawing of hard metals and alloys with a strength above 100 kg/mm2
(steels, nichrome, and others), and also for the hot-drawing of tungsten
and molybdenum. The standard specifies the most suitable shapes and the
most important dimensions of all types of diamond wire-drawing dies, per-
mitting wire-drawing with minimum power, minimum pressure, and best lubri-
Card 1/2

Diamond Wire-drawing Dies. rOr-7' ~'271-6~' S/ 0 2 01" X; c
(GOST 6271-60). Valid as From January 1, 136.' B020~BO58
cation. When ordering wire-drawing dies, wire tolerances must also be men-
tioned, owing to the fact that the standard rl(T 2771-57 (COST 2771-57)
specifies three to seven classes of tolerance Zor cold-drawn wire. The
histograms of the "Elektrokabelf" Plant, "Moskabell" Plant Moskovskiy
elektrolampovyy zavod (Moscow- Electric Lamp Works), and others show that
the moot suitable diameter of diamonds with a weight from 0.12-0.20 carat
is 0-15-0-35 mm for the purpose mentioned (Figs. 1-3). Theoretical studies
by the NIIAlmaz (Nauchno-issledovatellskiy institut almaza (Scientific
Research Institute of Diamonds)) served as a basis for determining 11
weight groups of diamond crystals as dependent on the diameter of the wire-
drawing die opening. A nominal weight and maximum weights of the diamonds
correspond to each weight group, from which a number of dies with various
diameters of the caliber zone can be manufactured (Table 2). The demands
made on diamond crystals are describs~d in detail, and the equation
d =Y~3 6 (G/y)' is given for calenilating the mean diamter of drawn wire
of 0-03 mm diameter and less, after weighing a wire of 200tO*1 mm with
an accuracy of + 0.00001 g, G being the weight of a 200 mm long wire
expressed in g, and y the specific gravity of the wire metal. There are
3 figures and 2 tables.
Card 2/2

SMIRNOV. G.D.; VINOGRADOV, P.M.; BYKOV, K.M.. akademik.
Gomposite electrical activit7 as one of the characteristics of the func-
tional condition of the cerebral cortex. Dokl.AX SSSR 91 no.2:433-436 JI
153. (MLRk 6:6)
1. Institut morfologii shivotnykh Im.A.N. Severtsova Akadeaiya nauk SWR.
2. Akademiva nauk SSSR (for Bykov). (Blectrooncephalography)
0

VINOGRADOVP;iMe.
Acetylene generatoro. Standartizatiiiiia 25 no.2:47-48 F 61.
(MIRA 14:3)
(Acetylene genera tors-StandarcloL)

SHIRMOV, G.D.;VINOGR&MV. P.M.
Electrical an-tion as one of indexes of cerebrocortical function.
Doklady Akad. nauk SSSR 91 no.2:433-436 11 July 1953- (CIXL 25:1)
1, Presented by Academician K. H. Bykov 12 May 1953. 2. Institute
of Animal Morphology imeni A. N. Severteov, Academy of Scleaces USSB,
1\1

VIVOGRADOV telia 24 uo.11:36-39 v 160.
Diamond draving dies. Standsrt'za (MIRA 13:11)
(2i.. (gtalworking))

eration o
'r Ij 0.
:,tructior. f, 25 no-?:
J.. rrriazi
Systeras. Vent*
wirt, N! 18:8)
J1 165. I.ele-
'Oroch"'kOy
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fr"InCy '1*1 . I . ~ .

V rNO:I-tkf)-)V, I - N. , Jt. a,i.
Low-rower radio stations in tne c-)al industrY. Popk'vn, U.mlete!fhlzdqt, 1~,49. 1`14- r.
(50-20458)
T1434 3. F6

TINDGRAWY, P.N.; LAZA I V. I.
B.MiRunmanev's article wOrgwdz4Ltion principles of telephone communicationO.
(From OUgel" u9sq, 1954) ugoll 31 no.4:38-39 AP 156. MHA 9:7)
(Kiue communica;ion) (Pumanev, B*No)

e
VINOGUDOV? P-N'
- I . n, of rural- I-,!-. ! )
. c,r devulOPme . and imp r (~-, Rk I - I
Toward fur'?~ 4, n-3.6; 2:-2 Je 16/..
37stems. vee".. 57ia7 A- 2 gorodskoY I ,Il,k3y tel-sfOnnO7
1. Narjhr,..j'nik Gla=090 upravlOril-Fa Ii SS5R.
s,rja%j 1 rad-lofikataii Hinisterstva GVY'%

USSR / Farm Animals, Small Horned Stook# Q-3
Abs Jour: Ref Zhur-Biol., No 12, 1958, 54795.
Author
Inst :Not given.
Title :On the Anatcmy of the Brain and Brain Membranes
of the Karakul Sheep.
Orig Pub: Nauchn, tr. Uzb. s.-kh, in-t, 1956, 10l 195-197.
Abstract: The brain of 12 Karakul sheep was studied mac-
roscopically. It was established that the aver-
age length of the brain is 8 to 8.8 am., length
of the cerebral hemisDheres - 6,5 to 6.7 am.,
length of the cerebellum - 2.5 to 2.8 am., its
width in the region of cerebral hemispheres -
5.6 to 6.3 am., length of hypophysis - 1 to 1.2
cmo, and its width - 0.5 to 0.6 am. The pecu-
liarities of different parts of the brain, as
well as of its membranes and of the cranial cav-
ity, are described.
Card 1/1
45

i1ploGIUMV, P-
Grindina and POUSh!09
Univeraal sina Illllvicf,'
NO . 3, 1953
f01. irts undo" t,.sto anI1,10s-
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Library Of Gjnyas5) June
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VINOGRADOVS starshiy prepodavatell
Lowering production costs and increasing the profit margin in the
petroleum production enterpriseSof the Kuybyshev Economic Council.
Trudy MIMiGP n0-30:29-61 159. (MIRA 14:5)
(Kuybyshev Province-Oil fields-Production methods)

FMONARMO, A-V., Ispolnyayushchly obyasannosti doteenta-, VIROGRADOV, P.V.;-
starshly nauchzWy notrudaik; HIKUTLOV, X.G., agronom-entomolog;
ITZRUSALDISXATA, X.F., studentka
Controlling soil posts in chockroved corn fields* Zashch. rast*
t wrods i bol. 5 no*4t24-~7 AP 160. (MMA 13:9)
:
. Rostovskiy universitat (for Ponomarenko, Iyerusalimakava),
..Zernogradakaya selektsionmaya stantsiya (for Vinogradov).
3* Sallskly nablyudatel'DYY punkt (for Kikhaylov)*.
(Corn (Maize))-Diseases and pests)

VINOGRADOV, P.V OLMIKOV, M.L.
Faulty design of the Tiahleev rat trap. GIg. i man. 24 no.9:86 S 159.
(KIRA 13:1)
1. Iz Nalitingradekoy oblastnoy sanitarno--epidemiologichookoy stantsit.
(RA.TS--XrLMMIITATIOT)

8(5), 18(5)
SOV/ 112-59-4-7 128
Tranalation from: Referativnyy zhurnal. Elektrotekhnika, 1959, Nr 4, p 101 (USSR)
AUTHOR: Xilnogradov, P. V.
TITLE: Testing a Water-Lifting Electrical Winch for Deep Wells
PERIODICAL: Tr. Turkm. 9.-kh. in-ta, 1957, Vol 9, pp 159-176
ABSTRACT: Bibliographic entry.
Card 1/ 1

VNOGRADOV, P.V., nauchnyy sotrudnik
-1 .- . I
Eliminate discrepancies. Zashch. rnst. ot vred. i bol. I no.1:45-46
jA-F 158. (MIRA 11:3)
1. Zernogradakaya selektsionneyn Rtantaiyn.
(Tiants, pxotection of )

"Y
USSR/Ctativated Plants Grains m-4
Abs Jour Ref Zhur - Biol., No 1, 1958, No 1514
Author Jj..~~ov
Inst Not Given
Title Reasons for the Scarcity of Young Corn Crops in Kidus
Orig Pub Kukuruza, 1956, No ~,, 17~-lq
Abstract The data from 5 areas investigated in two "kolkhozes" of the
Sla'skiy Rmyon (Rostovskaya. Oblast' in 1956). The amount of
empty aidus of the young corn crops depends on the non-sifting
of seed by soving machines (2-8%), the trimming of plants by
cultivators (6 - 8%), seed dw=ge through disease (4 - 10%),,
injury by soil p,3sts (6 - 10%) and less through birds and
Siberian marmots (when the crops are still in their early
stages).
Card 1/1

VINOGRADOV, P.V., nauchnyy sotrudnik
Chibk-pea miner Uriomyza cicerina. Rd. Zashch. rest. ot vred. i
bol. 4 no.5:56 S-0 159. (MIRI 16:1)
(Rostov Province-Chick-pea--Diseases and pasta)
(Rostov Province-Leaf miners-Extermination)

VINOGRADOY
, nauchnyy sotrudnik; MALYAROV, V.ye., agronom
In the Sal Steppes. Zashch.rast.ot vred. i bol- 3 no.6:25-26
N-D 1 58. (MRA 11:12)
1. Zernagradakaya goeselekstantelya, (for Vinogradov). 2. Kolkhoz
Imeal Stalina, Sallskogo rayona. Rostovskoy oblasti (for Malyarov).
(Sal Steppe-Agricultural pests)

VINOGRADOV, P.V.
Millet
Foxtail millet pests and their control, Sel, i Sam., 19, No. 4. 1952~
Month3,v List of Russian Accessions., Library of Congress,, June 1952. Unclassified.

VINOGRADOV, P.V.
Insecticides
Foxtail millet pests and their control. Sal. i sem.0 19, No. 4.. 1952.
Monthly List of Russian Accessio.is,, Library of Congress, June 1952. Unclassified.

VINOGRADOV., P.V.
Agricultural Pests
Foxtail millet pests and their control. Sel, i sem. 19 No. 4 s 1952,
Monthly List of Rumbian Accessions Library of Congreas, June 1952. Unclassified.

i . VILOGRADOV, P.V.
2. USSq (600)
4. Wheat - Diseases and Pests
7. Damaging of spring wheat by the seed-eating tychius. Sel.i sem. 19 no.10,
11952.
9. 'Monthly List of Russian Accessions, Library of Congress, January 1953, Unclassified.

1. VINOGRADOV, P. V.
2. USSR (600)
4. Weevils
7. Grain weevil. Priroda 41 no. 10, 1952.
9. MonthlX L,.st of Russian Accessions Library of Congress, February 1953, Uncla:3sified.

-.7
-- --- -1-1 -
Or. Jet Propulsion Engines "- K. E. Tsi lkovsky,
Theorist, Designer (Co-Author)
Soviet Source; P; Ogonek #18 MUY 46, Moscow
Abstracted in LUAF "Treasure Island".. on file In
Library of Congress, Air Information Division,
Report No. 82022

AID P - 1818
Subject USSR/Aeronautics
Card 1/1 Pub. 35 - 13/18
Authors V~no 4 Eng. Major, Dotsent, Kand. of Tech. Sci.
-49WORMYS04A, Eng.
I
Title Soviet jet aircraft fighters
Periodical Vest. voz. flota, 3. 68-78, Mr 1955
Abstract The author gives a short history of the development
of fighter aircraft In Russia from 1915 UP to recent
times. The MIG-15 is described as the last aircraft.
Diagrams, graphs and photos.
Institution: None
Submitted : No date

---- - -- - - -- - -
ff-837 (A process of successive approximations for finding characteristic values and
characteristic vectors) Protsess posladovatellnykh priblizhenii dlia otysk-niia
sobstven:qkh. chisel i sobstvennykh Yektorov.
DMMM AKADEMII NkUK WSRt 83(2): 173-1749 1952.

Vest, "o. 0, 71-
An Outsta:-.d;--,- So--Let Sc-'I;ant-!-~", (The 61~'h '-LnLv~rsary of V. 11.
A rlort ou'Uno of the activ, 4. 0
L U.
50: Pef --~ra+.j!.rn7-?' ZLurij-i~- 01-30q~07)

VIIMGRkWV, R. and MDIAYEV, A.
"Soviet Jet Fighter Planes'. " Vest. Vozd. Flot., No.3, pp 68-78, 1955
Translation F-TS-8576/V

VINOGRADOF R., kandidat tekhnicheeklkh nauk; ZAYTSIV.V., kandidat
-'ft
FeRT c skikh nauk
T&K-18 airplane. Kryl. rod- 3 no-1:22-24 Ja 152- (NLRA 8:8)
(Airplanes)

T
AID P - 264f
Subject USSR/Aeronautics
Card 1/1 Pub. 135 - 2/17
Author Vinogradov, R., Major Eng., Dote., Kand. Tech. Sci.
Title Tsiolkovskiy, K. E. and contemporary aviation
Periodical : Vest. vozd. flota, 9, 9-16, S 1955
Abstract : A brief review of Tsiolkovskiy's work, mainly in the
field of rockets and jet-propelled aircraft.
-istitution : None
Submitted No date

VINOGRADOV,R.; ZATTSIV.Y.
Scientist-innovator. Kryl.rod. 2 no.6:10-11 is 151.
(NLIA 8;8)
(Yetchinkin. Vladimir Petrovich, 1888-1950)

VD;C-GRADU, -R-.
Z "Aerial" type of Jet-Propulsion Engines
Soviet Source: P: Ogonek #18 (Moscow May 46)
Abstracted in USAF "Treasure Island". on file in Library of Congress, Air Information
Division, Report No. 77574.

VINWRADOV-1 R.- (CO-AUTHOR)
On-Helicopter "TsAGT I-EA", and others; designers Yurlyev and Bratukbin
Soviet Sources P: 0gonek # 20, Moscow May 1946
Abstracted in USAF "Treasure Island", on file in Library of Congress, Air Information
Division, Report No. 77798.

VINOGRADOV, R.A.
Machine tool unit with a liftirg table. Biul.tekh.-ekon.inforn.
Goo.nauch.-iorl.inst.nauch.i tekh.inform. 18 no.1:31-32 Ja 165.
(MIRA 18:4)

--IV[,NIY',.f(ADOVJI R.I.; LENIKO, O.N.
-,Jmlating thin-walls:.-d structures working in an elastrpllt3ric
defomttion zone during h#~at!ng. Tzv. vyn. uchnb. zav.; av.
tekh. 7 no.3:52-58 165. (MIFIA 18:9)

Aravzu"at) ViWILM buultuz k;VL)z: UJK/U147/U0/UUU/UVa/Uu0z/U'~bt5
AUTHOR: VinwadoV, R. -1 ;.Len1ko, 0. N.
ORG: None
TITLE: Modeling of thin-~walled structures operating in an elastio-plaBtIc deformation region
subjected to heating
SOURCE: IVUZ. AviatBionnaya tekhaika, no. 3, 1965p 52-68
TOPIC TAGS: aerosRace struq~, supersonic aircraft model scaling, elastic deformation,
elastic stress, plastic deformation, thin walled beam
ABSTRACT: EarIl er the authors (Odvukhmasshtabnom modeffrovanii tonkostennykh konstrukt-
siy. M., 115trultellnaya mekhanika I raschet sooruzhenly," No. 1~ 1963) examined the similar-
ity criteria for thin-walled structures without heating. The present artic1l amines the
similarity condition In the case of heating in the elastic-plastic deform att=gion, which is
characteristic of structural components of supersonic vArcraf . The similarity criteria of
plastic deformation under dynamic load and the effect of steady-state heating are employed, as
are the similarity criteria of elastic deformation under dynamic load and the effect of non-
steady-state heat!RKIWhe fundamental equations of plasticity theory and the dynamic equations
of equilibriuii -and-&fori-ation from elasticity theory pe employed to derive the similarity
criteria. Orig. art. has: 23 formula-. 4Y
UDC: 539.3+629.13. 01
SUB CODE: AS SUBM DATE: 18Feb64 / ORIG REF: 004 OTH REF: 001
ard
C
-1/1

E.'T (~j "m I- ~'E_,'; F"T-
ACCESSION 1; ft AT'501555.~ 0 n20 q o S 9 8
[AUTHORi Vinogradov, R. I.; Vinogradov, 1. N.
TITLE i Automatic flapping wing. Class 62, No. 170305
SOURCE: Byul leten ' izobreteniy I tovarnykh zn akov , no . 3 , 1965 98
!TOPIC TAGS: flapping wing, flapping wing glider, airframe component
'ABSTRACT: An Author Certificate has been issued for an automatic
,flapping wing for gliders. It consists of a nose section outfitted
with ribs, tail section, double-wall and auxiliary longerons, dove-
,tailed blades flexibly mounted on the streamlined ribbing, and com-
iponents for joining the wing to the fuselage. A gervoactuator Is
!mounted on the double-wall longeron for the purpose of maIntaining
the center of gravity of the o9cillating ving frame at 8 point neAr
the longeron axis, for Increa;ing the dynanic properties of the wing
and for assuring damping. This servoactuator Is connected to a
,reducer and weight balance which produces the automatic oscillation
Card 1/2

L 55020-65
ACCESSION NR: AP5015554
of the wing. The initial oscillating impulse is given by a pneumatic
cylinder rod through a support disk fastened to the auxiliary longeron.
The panel of the wing is hinged to the fuselage by a bracket connected
with a horizontal damper and with a shock-absorber rod. w1i
ASSOCIATION: none
SUBMITTED: 25Nov63 ENCLi 00 SUB CODE: AC
NO REF SOV: 000 OTHERt OGO ATD PRESS: 4027
2/2

86-58-4-16/27
AMOR: Vinogradov, R. I., Engineer, Lt Col., Docent.. Candidate of Tech-
n1cial -Sciences 1w Bogdanav, A. P... Engr-Capt
TITLE: Aerodynamical configuration of a Supersonic Aircraft (Aerodyna,
micheakaya kamponovka sverkhzvukovogo samoleta)
PERIODICAL: Vestnik vozdushnogo flota, Nr 4; 1956, PP 55-63, (USSR)
ABSTRACT: First the author discusses the general peculiarities of the configuration
of a supersonic aircraft and presents in Fig. 1 a table of classified
aerodynamical configuration of such an aircraft based on two mainfea-
tures: the configuration of the wing and the arrangement of the empen-
nage. He divides the whole range of speeds into subsonic, transonic,
supersonic and hypersonic regions and describes each region seperately.
He indicates that the transition fram subsonic to supersonic speeds is
bound with the problem of overcoming the additional (wave) resistance
which increases greately in the transonic region, and that the character
and the magnitude of the change of the coefficient of wave resistance of
an aircraft, with respect to velocity, depend on the wave resistance of
the parts and their location on that aircraft.
Card 1/3

86-58-4-16/27
Aerodynamic Configuration of a Supersonic Aircraft
The author also discusses how the fom and the aspect ratio of a wing, the form and
relative thickness of an 94rfoil a;ffect the character of the flow of wave resist-
ance of a wing. In Fig. 2 he presents a diagram showing the dependence of the coeffi-
cient of head resistance'"Of an aircraft on M at zero lift force. In Fig. 3 the
graph shows the interdependence between the relative thickness of the airfoil and M
critical for an arrow a~d a rectilinear wing. In Fig. 4 he shows '
the influence of tbe reliLtive thickness of airfoil on the coefficient of wave resist-
ance at its maxium value.
Further the author analyzes the aircraft with respect to their wing form. He amL,
.4-meseperately various aircraft, aircraft with a triangular wing, rectilinear wing,
arrow wing, an aircraft with a wing in the form of a ring (Fig. 5), an aircraft with
a circular wing (aircraft-saucer Fig. 6), an aircraft without a horizontal empennage
(tail-less aircraft or'flying wing), an aircraft with the horizontal empennage located
in the rear, and an aircraft with the horizontal empennage located in the front.
.(aircraft-ducQ
Finally the author mentions the constructional. changes in the wings which should im-
prove their aerodynamical characteristics during take-off and 3-ding at low speeds
and which he calls the mechanization of the wing. He discusses also the following
Card 2/3

86-58-4-16/27
Aerodynamic Configuration of a Supersonic Aircraft
prospective means of mechanization of supersonic aircraft: the jet flap, the control
of the boundary layer, the variable sweep-back of the wing (Fig. 7), and the varia-
tion of the angle of a wing's setting.
There are three schematic drawings, three diagrams, and one photo.
AVAPABLE: 'Library of Congress
1. Airplanes - Suporscnic characteristic4 2. Airfoils -
Supersonic characteristics 3. Airplanes - Aerodynnmic
characteristics
Card 3/3

MM I BOOK MUW3!rATION SOV/5826
Vinogradov..'R6stislar Iyanotich.. and Aleksey Vasillyevich Minayev
Samolety SSSRj* kratkiy ocherk razvitiya (Aircraft in the USSRj a Brief Outline
of Their Developwnt) 2d ed,,:rev. and enl, Moscow, Voyenizdat X-va obor,
SSSR., 1961, 297 p. 3-1.9500 copies printed*
Ed,: If, P, Gordeyev; Tech. Ed.: To F. Njasnikova.
PMUIOSE: This book is intended for students at aviation schools.. flying and
technical personnel of the Soviet Air Force., Civil Air Fleet, and All-Union
Voluntary Society for the Promotion of the Army,, Aviation and Nsvyp and for
general readers,
COVERA(Z., The book Is concerned primarily with the development of airplanes under
the Soviet administration. Oho I, vhich deals vith the invention of the air-
plane and the beginnin of Russian airplane constructioupcontains information
on A. F. Nozboyakiy., vho., according to the authors,vas the inventor of the air-
plane. Only typical airplanes and those vhich have contributed to the develop-
ment of aircraft designs are presented. Photogjayhs~ drdwings*., and doncied
"_% -1/ -5 -

Aircraft In the USSR (-ont.)
SOV/5826
performnce characteristics of some airplanes an Included, The authors have
drawn mach of their source material from the Tsentrallnyy Gooudarstvenny
voyenno-istoricheakiy arkhiv (Central State Archives of Military Hictory~ and
the Tsentrallnyy Gosudarstvennyy arkhiv Krasnoy Armii (Central State Archiw-e
of thl Red Army), No personalities are mentioned, There are no refeL*nces,
TAJ31Z OF COMMITS:
Preface
i
3
Ch, I, Invention of the Airplane and the Beginning of Russian
Airplane Construction 5
The im.ntlon of the first.airplane 5
The Inception of aeronautical science 17
Besd-lm of Russian airpla construction
Ch. 31, The First Heavy and Maneuverabj* Airplanes 29
Developing helivy airplanes 29
Deve3,oping light manewemble airplanes 35
Developing seaplanes 42
The development of Russian aeronaittical science 43
Card 2/5

VIVOGRAM9 Rost islml~ovich; HINATEV, Aleksey Vaell'yerich; PISARKV, U.S.,
I ~-rlili~;_"C-4p%lm ~
n aner- ornik, redaktor; SOLCKCWIK, R.L., takhnicheekly red&ktor.
M
(Brief study of the development of airplanes in the U.S.S.R.] Kratkii
ocherk razvitiia samoletov v SSSR. Moskva, Vosa. isd-ve Ministerstva
oborony SSSR, 1956. 254 p. (MLIU 9:5)
(Aeronautics--History)

ACC NRi AP6035934
SOURCE CODE: UR/0413/66/000/0---,J/0196/0197'
INVENTOR: Vinogradov, I. N.; Andreyev, V. M.; Vinogradov, R. I.
ORG: none
TITLE: Flapping-wing motorcycle (Engine-powered ornithopter mounted on a motorcycle
frame]. Class 62, No. 187533
SOURCE: Izobreteniya, promyshlennyye obraztsy, tovarnyye'znaki, no. 20, 1966,
196-197
TOPIC TAGS: xlxizxgx, STOL aircraft, research aircraft, unconventional aircraft,
ornithopter
ABSTRACT: An Author Certificate has been issued for an engine-powered ornithopter
resembling a monoplane equipped with a folded flapping wing with feather-like blades
on the tips. The wings are mounted on the frame of a motorcycle together with a
horizontal tail unit, control vanes, a drive, and a system of mechanisms for
effecting their flapping motion. To increase wing efficiency, between the feather-
like blades' drive gear and longerons is a mechanism for automatically changing the
blades' angle of attack; this mechanism consists of a support (articulately attached
to the first section of the wing and connected by a pull rod with a lever on the
drive shaft) and a round deflecting balancer (attached to the traverse of the end
rib of the sacond section of the wing and attached to the support through a ball, and
UDC: 629.135/138

the other end is connected vith to the crank of the second wing section, which is
connected by pull rods with the longerons of the feather-like blades). In order to
free the drive mechanism of the wing's natural vibrations, a compensating cross-piece
~uspensi6n is used, which is connected by a pull rod with the drive-rachanism.cam;
at the other'end it is connected to a cantilever of the first section of the wing.
Orig. art. has: 1 figure.
SUB CODE; Ol/ SUBM DATZ:'3ODac64

I.
VINOGIULDOV,,R., inzhener-mayor; ZATTSLV, V., inzhener-mayor.
Soviet all-metal airplanes. Tent.Vozd.71. 34 no.12:57-67 1 151o
(Airplanes-Design and construction) (MMA 8:3)

moomm,-R, and 14INAYEVt A.
"Soviet Jet Figbter Planes," Vest. Vozd. Flota, No.3, pp 68-78, 1955
Summwy of article D 306363, n jul 55

I )I
ik' 14
AID P - 4990
Subject USSR/Aeronautics - bibliography
Card 1/1 Pub. 135 - 18/26
Author Not given.
Title Development of airplanes in our country
Periodical Vest. vozd. flota, 9, 81, S 1956
Abstract Critical review of the book Kratkiy Ocherk Razvitiya
Samoletov v SSSR (Short Outline )f :D-e-v-eYo-p-TCe-nt of
Airpla Tn--UMR), by R. 1. Vinogradov, A. V. Minayev.
Published by the Defens'e-4"1tft*tr?nrVr-WR, Moskva, 1956,
256 pages.
Institution : None
Submitted : No date

S/143 62/000/012/004/005
D238YD308
AU T 110 R it.I., candidate of Technical Sciences
TITLE: The aerodynamic characteristics of a windwheel with
self-oscillating blades
PITUODICAL: Izvcs-4iya vysshikh uchebnykh zavedeniy. Energetika,
no. 12, 19621 86-94
MNT: Experiments were carried out in a closed-jet wind
tunnel on irindwheel models with normal (fixed) blades and with blades
fitted flexibly, to: (a) demonstrate any advantageous dynamic effect
occurring as a result of steady-state se If- oscillations of the blades
and (b) ?bring out the possibility of opo-rating windwheels with oscil-
C.~
latincy blades without prejudicing mechanical strength and irithout
CR CD V
inEringing the safety of the operating personnel. The cxn)erimental I/
windwheels had a diameter of 0.6 m, carrying 3 blades and with a sin-
gle-component blade oscillation (torsional oscillations). The blades
were mounted freely on the hub by a flexible coupling providingf steady-
state oscillations of the blades at wind speeds as low as 3 m/sec.
Card 113

S/143/62/000/012/004/005
'rho acrodynarnic cl.iaracterist-ica ... D238/D303
The following parmeters were mca-,urcd during the experimentS: speed
C3
of the windufficel; torsional displacements of the blades and the or,-
cillating frequencies; time variation in the moment of the windwheel;
variation in the stream velocity in the wind tuni-ml in front of the
Windwheel. It was found that se If- oscillating blades on liigrh-spe~d
wind machines result in a higher starting and run-up characteristics
C3
of the high-speed izindwhcel approach -those of the slow-speed wind-
wheel employing the normal typc of blande fixing. "elf -oscillating
blades thus combine in one unit the properties of high and low-specd
windwheels and extend the range of high-speed wind machines. -~'elf-
C_V
oscillating blades increase the wind utilization factor on averct-c
by 15 to 20clo, depending on the angle of advance. variation of the
stream, or wirkI velocity has practically 'no effect on the amplitude
of steady-state oscillations. The self-oscillations collnpsc with a
very sharp increase in the irind-streaTa velocity. 'The sel.-E-osciM,4-
tior, conditions can be regulated by means oil movable equalizers or
int,.!rchangeablc flexible elements. Blades Trith freely or flc-.-.ibly
mr-inted wing flaps on the trailing edge of the vane provide a lower
c:-4-Lic--l self-oscillation speed, which favorably influences the
( =d 2/3
L

I S/Ili3/062/000/012/004/005
The acrodynamc characteristics ... D233/_IJ308
starting moment. TIe theoretical -and experimental data point to the
possibility of employing blade self-oscillation for the pux~pose of
improving the aerodynamic characteristics of i-rindwheels. There are
7 figures.
SUBI-11TTED: January 9, 1962-
Card 3/3

VINOGRADOV, R.I., kand.tekhn.nauk; KUVYCHKIN, V.I., inzh.
Racing boat with underwater wings. Sudostroenie 28 no.6s5l
Je 162. (MIRA 15:6)
(Planing hulls) (Motorboats)

\ It z-,, , " ; - .-" j-,-- - T,I\k
. T-,, - -1 _-,, ~ , V jj
V f_ I i ~ I
1(2);1(3) PHASE I BOOK EXPLOITATION SOV/2307
Bogdanov, Aleksandr Pavlovich, Rostislav Ivanovich Vinogradovp and
Konstantin Dmitriyevich Mirt
Sbornik zadach po konstruktsii i proc 'hnoBti samoletov (Collection of
Problems on Aircraft Constructipn and Strength) Moscowp Oborongizp
1959. 230 P. Errata slip inserted. 7,000 copies printed.
Reviewer: Kh. S. Khazanov, Candidate of Technical Sciencesp Docent;
Ed-: A.M. Yarunin, Engineer; Ed. of Publishing House: L.A.
Beiyayeva; Tech. Ed.: N.A. Fukhlikova; Managing Ed.: A.I. So-
kolovp Engineer.
PURPOSE; This text book was approved by the Ministry of Higher
Education of the USSR for studentSof aeronautics vuzes and depart-
ments.
COVERAGE: This collection of problems on the design and Btrength of
aircraft was compiled for the courseE "Strength analysis of air-
Card l/ 4

Collection of Problems on Aircraft (Cont.)
SOV/2307
craft" and " Construction and design of aircraft". It is intended
to aid students to solve engineering and analytical problems under
the supervision of instructors and independently.
TABLE OF CONTENTS:
Procedural instructions 3
Ch. I. Forces Acting on Aircraft 5
1. Forces and overloids acting on aircraft in flight 5
2. Flight loading conditions and maximum characteristics 20
lCh. II. Wing 27
1. Wing load and stresses in wing sections 27
2. Calculations for frame elements 45
3. Stresses in wing sections 51
4. Analysis of wing components 66
Ch. III. Aileronsp Empennage8, Control 102
1. Ailerons 102
2. Tail unit ill
Card 2/ 4

Collection of Problems on Aircraft (Cont.)
3. Control
Ch. IV. Empennage and Wing Vibration. Aeroelasticity
Ch. V. Fuselage and Engine Mounts
1. Fuselage
2. Engine mounts
Ch. VI. Landing Gear
1. Analysis of shock absorbers
2. Strength analysis of landing gears
Ch. VII.. Aircraft Control
SOV/2307
u6
125
130
130
151
160
16o
168
178
Ch. VIII. Emergency Crew Rescue Devices, Air-tight Cabins, De- 0^
termination of Aircraft Parametersp and Centering 109
Appendixes
Card 3/ 4

Collection of Problems on Aircraft (Cont.)
I. Table of the International Standard Atmosphere
II. Characteristics of Aeronautic Airfoils
III. Graphs for Longitudinal Bending Analysis of Bars
SOV/2307
196
199
218
228
13/bg
9-18-59
IV. Values of the Coefficient k in Relation to Conditions of
Support and Loading of Plates
AVAILABLE: Library of Congress
Card 4/4

VIN'0GRkWV, R.I. (Riga)
Relationship between parameters of the vnrtax Inverted
path and Strouchal's number. Izv.vyR,uchab,zav*; Uvotokh*2
no.4:14-25 ,p. (MULk 13: 4)
( ortex motion)

VINOGRADOV, R.I., inzh.-podpolkovnik, dote., kand, tekbu. nauk; BOGDAWT,
-- - , -----A'X., Insh.-kapitan.
Aerodynamic composition of supersonic plans, Test. Tozd. Fl. 40
no.4:55-63 Ap '58. (MIRL 11:4)
(Aerodynamics, Supersonic)

s/ii5/62/00o/oo6/003/005
AUTHOR: V
TITLE: A new design of strain gauge pressure transducer
PERIODICAL: lzmeritellnaya tekhnika, no.6, 1962, 20-23
1 0. "t, ~ -,I'.
TEXT; Small cylindric !wir '"a-strain gauges may be used with
normal strain gauE jkh" d
-03-cfe an recording on an electromagnetic
pressures. The
oscillograph to measurii 'Idiy changing gas
sensitive element is a slio"A thin walled cylinder supported.by
constantan wires. Away from the supporting frame, changes of
pressure alter only the tension in the thin walled cylinder and
gauges, whilst near the frame there is also bending and the short
cylinder is affected by bending over its entire'length, which
increases the sensitivity. - Approximate formulae are given for
selection of element geometry to ensure high sensitivity and indeed
the sensitivity is appreciably higher than that of membrane type
gauges of similar size. Also, the now gauges are more reliable.
Constantan wire 0.03 mm diameter is wound lengthwise on a
cylindrical frame to which an elastic film is then secured to
form the cylinder. For pressures in the range from 0.0001 to
Card 1/2

S/115/62/000/006/003/005
A now design of strain ... E194/9435
10 atm, rubber or polyethylene tapes are used, for higher
pressures smooth or corrugated metal foil is used. For pressures
above about 1 atm. wires are wound around the cylinder as well as
lengthwise. The wires are wound with some initial tension to
improve the frequency characteristics and stability.
A differential pressure gauge is-described which employs two
elastic cylinders; gas at one pressure is delivered to the space
between the cylinders and at the other to the surrounding inner
and outer spaces. Practical design recommend ons are made for
10
pressure gauges to suit various conditions of u and pressures
including recommendations concerning optimum fr ency in relation
r ~
nj*
to gas conditions and the type of oncillograph ments used.
S,tatic and dynamic calibration, the latter usin crank driven
T
piston arrangement, are briefly discussed. he are.4 figures.
Card 2/2

ACC NRi
kP6036857 SOURCE CODE: UR/0147/66/000/004/0068/0074
AUTHOR: _Yin
Ig!adov R. 1.
..........
ORGt none
TITLE: Using the method of variation of sindlarity-constants In the project design
of aircraft-
SOURCE: IVUZ. Aviatsionnaya tekhnika, no. 4, 1966, 68"74
TOPIC TAGS: aeronautics, research aircraft, aircraft teat, test model, model
scaling, model test, similarity theory
ABSTRACT: A method of varying similarity constants for the analysis of aircraft cqn-
figurations is outlined which makes it posqible to obtain a great number of near
configurations with oscillating elements~l/'~fhis method consists In varying the
similarity constants with respect to defining parameters, that is, those which are
contained in similarity criteria of the phenomena considered here. In this case,
is is possible to go from an initial model through the entire spectrum of con-
figurations differing structurally from one another but able to operate regularly#
This makes it possible to select the optimal configurations from those obtained and
to use the results obtained from one model for carrying out design calculations for
structurally different configurations. This method is applied here to the analysis
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ACC NR' AP6036857
of aircraft configurations with an oscillating element (semirigid ving or Its secr
tion). The ddrfining parameters are frequency characteristics of the model. Three
types of configurations are presented as an illustrative examples Orig. art. has:
5 figures and 11 formulas.
SUB CODE: Ol/ SUBM DATE: 28Dec651 OkG PEFC 004/ ATD, Ppzss: 51o6

.,VINOMWOVj Rctislav Ivanovich; MINAYEV) Aleksoy Vasillyevich; GORDEYEV,
red.;- IdASNIXOVA) T.F.0 tekhn. red.
(Airplanes of the U.S.S.R.) SamoletY SSSR; kratkii ocherk razvitiia.
Izd*2*p perer, i dop. Moskvaj, Voen. izd-vo M-va obor. S&T., 1961.
297 p, (Airplanes) (MIRA 14:3-1)

le
ci

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AUTHORt -,-Vinogradov, R.I. (Riga)
TITLEt Relation of the Parameters of the Inverse Vortex
Street and the Strouhal Number
PERIODICAL: Izvestiya vysshikh uchebnykh zavedeniy, Aviatsionnaya
tekhnika, 1959, Nr 4, pp 14-25 (USSR)
ABSTRACT In determining the forces which act on a win\ at constant
amplitudes of oscillation in plane incompressIble flow,1
it is convenient to use the hydrodynamic analogy ol=e
vortex wake suggested by Golubev (Ref 1). A chessboard
vortex street forms behind the wing similar to the drag
vortex street but with an opposite sense of rotation.
The basic parameter of the inverse vortex street (ratio
of street width to vortex pitch) is independent of the
Strouhal Number in a given range of Reynolds Numbers and
is equal to 0.281 for any oscillation law, The street
width is equal to the oscillation amplitude. The
velocity of the vortices in obtained from the formula
for the drag street by substituting the inverse rotation
in the Karman formula. These assumptions have proved
Card 1/3 valid only for special oscIllations. Generally, the

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Relation of the Parameters of the Inverse Vortex Street and the
Strouhal Number
drag and lift of the oscillating wing can be obtained
by substItuting a function of the Strouhal Number for
the width/pitch ratio and another function for the
vortex velocity. It follows from experimental
evidence that the width/pitch ratio and the vortex
velocity are pronounced functions of the Strouhal
Number in the range of 0.05 to 1.0, that the width/
pitch ratio varies in time for each pair of vortices and
that, generally, the 4mplitudes of oscillation are
substantially smaller than the vortex street width.
The interpretation of many frames obtained by motion
photography has shown that averaging does not give a
true picture. Different mutual dispositions of vortices
exist at different instants of time. The wake
oscillates about a mean position at the frequency of
wing oscillations. With zero phase between the torsional
and flexural winf oscillations, the chessboard pattern
vanishes. At 90 phase, the most pronounced inverse
Card 2/3 vortex streets are observed. The life of a pair of Y

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Relation of the Parameters of the Inverse Vortex Street and the
Strouhal Number
vortices is divided into three periods. In the first
period, the vortices are established and the street
widens; in the second period, the mean limiting value
of the width is maintained and in the third period, the
vortices diverge. A brief-analysis leads to a
formulation of the width/pitch ratio and the vortex
velocity as functions of the Strouhal Number. During
the first two periods of the vortex life, the pitch
.remains constant. The width changes in time an a
result of the viscosity of the flow. Analysis with the
formulae given in the paper yields to satisfactory
agreement with experiment and the derived value of the
width/pitch ratio can be used to compute the drag, lift
and efficiency of the oscillating wing in accordance with
the formulae of V.V.Golubev. There are 10 figures,
1 table and 3 Soviet references. LK
SUBMITTED: April 30, 1959
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PHASE I BOOK EXPLOITATION 161
Vinogradov., Rostislay Ivanovich, and Minayev, Aleksey Vesillyevich
Kratkiy ocherk razvitiya samoletov v SSSR (Brief Outlirrof Aircraft
Development in the USSR) Moscow, Voyen. izd-vo Min-va obor. SSSR,
1956. 254 p. No. of copies printed not given.
Ed.j Pisarev, M.S., Engineer-Colonel; Tech. Ed.: Solomonik, R.L.
PURPOSE: The book is intended for students at aeronautical
engineering schools and for the flying and technical personnel of
the Air Force and the All-Union Voluntary Society for the Promotion
of the Army, Aviation, and Navy.
COVERAGE:- The book contains a historical outline on the dovelooment
of Russian aircraft, beginning with A.F. Mozhayskiy's plane and
embracing contemporary high-speed jet aircraft. It was,compiled
from archive material; part of it was published before in magazines,
part Is published for the first time.' No personalities are
mentioned. There are 51 references, of which 50 are Soviet and 1
German.
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Brief Outline of Aircraft Development in the USSR 161
From the Authors 3
Ch. I. Creation of the Airplane and the Beginning of
Russian Airplane Construction 7
Creation of the-first-a-irplane 7
Birth of aeronautical science 24
Beginning of Russian airplane construction 31
Ch. U. The First Heavy and Maneuverable Airiplanes 41
Development of heavy aircraft 46
Development of light maneuverable aircraft 52
Development of seaplanes 59
Ch. III. Development of Bombers, Fighters and
Reconnaissance Airplanes 62
Heavy bomber biplanes 62
Maneuverable fighter-biplanes 73
Reconnaissance airplanes 86
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Brief Outline of Aircraft Development in the USSR
Reconnaissance seaplanes 89
Ch. IV. Beginning of Soviet Airplane Construction 95
The first Soviet airplanes 100
Beginning of all-metal airDlane construction 104
Ch. V. Establishment of the Soviet School of Aircraft
Design ill
,Heavy monODlanes 113
.Development of maneuverable fighter planes 137
Attack planes 149
Reconnaissance planes 150
Civil aircraft 155
Tra-ifting and special airplanes 159
Ch. VI. Development of High-speed Aircraft 162
The first high-speed monoplanes 162
161
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Brief Outline of Aircraft Development in the USSR
High-speed maneuverable fighter planes 169
From "air cruiser" to high-speed medium bomber 180
High-speed heavy aircraft 191
High-speed attack planes 196
High-speed civil aircraft 200
Ch. VII. Aircraft of the Second World War 207
Development of new combat planes 207
Development of combat planes in the course of the
Second World War 218
Ch. VIII. Postwar Aircraft Construction 235
AVAILABLE: Library of Congress ISIkBV
8-6-58
161
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