SCIENTIFIC ABSTRACT BOLONI, I. - BOLOTICH, I. P.

• Document Type: CREST
• Collection: Scientific Abstracts
• Document Number (FOIA) /ESDN (CREST): CIA-RDP86-00513R000206120009-1
• Release Decision: RIF
• Original Classification: S
• Document Page Count: 100
• Document Creation Date: November 2, 2016
• Document Release Date: June 9, 2000
• Sequence Number: 9
• Publication Date: December 31, 1967
• Content Type: SCIENCEAB

BOLONI, Istvan
RotarY moving machinea. Mazo-1. techn 1 no.4.2-3:~161.
Tw-

BOLOWI, Istvan
Maize combines h4ve passed the test. Mezogazd techn 1
no.9:12-13 161.

BOLONI, Istvan
Experience in the mechanization of husking Indian corn.
Mezogazd techn 1 no,11:20-21 161.

BOLONI, Istvan
Testing tractor grass mowers with small cutting width.Pt.2.
Jarmu mezo geP 4 no.1:1-4 Ap 157.
1. Mezogazdasagi Gepkiserleti Intezet.

BOIDNI, I.9tvan, dr., a muszak-i tudomar-riyok kandid-ttlisa
Pneumatic transportation of ground and chopped agricultural
products. J&rmu mazo gep 10 no.7:253-257 Jl 163.

BOLONIN, D. G., Cand Tech Sci -- (diss) "Forms of loss of dynamic stab-
ility, and longitudinal bending of rods occuring in action of explosive
loadings." Leningrad, 1960. 18 pp; (Higher Naval Order of Lenin Engin-
eering College im F. E. Dzershinskiy); price not given; (KL, 27-60,
152); number of copies not given

BOLONINO VASILJTY IVANOVICH AND M. F. TEPLIAKOV
ell- --- -- -- -- ---- - - -- -- --*--- - I---
Opyt otopleniia 1-arovozov drovami. Moskva, Transzheldorizdat, 1943. 56 -L. illus.
Using wood as locomotive fuel.
DLC: TJ648.B65
SO: Manufacturing and Mechanical Engineering in the Soviet Union, Library of Congress,
1953.

POGOSIANZ, H. E., BOLONI'._ , N. I. and OLSHEVSYAYA, L. V. (Moscow)
x -1 -.I
~,., ~ -- 1~,j -, )", /r1; -1 -
I, : i , I '.
"Ibe Steppe-Lemming (Lagurus lagurus Pall): A New Animal Suitable for
Cancer Research."
report presented at the 7th Intl. Cancer Congress., London, JulY 1958.

POGOSYANTS, Ye.Y BOLONRIA, N
Attempted demonstration of a tumor-prodUC4 '-Z agent in ext~r.acts of
human mammary cancer. Vope'onk. 4 no.4:)8-1--391 158 (MIRA 1199)
1. Iz laboratorii opukholevykh shtammov (zav. - doktor biol.nauk
Ye.Ye. Pogosyants) otdela etiolorii i pntogeneza opukholey (zav
deyatv. chlen AMN SSSR prof, A.D. Tinofeyevskiy) Instituta
eksperimentallnoy patalo-ii i terapii rak-a AMN SSSR (dir' chlen
AMN SSSR prof. N.N. Blokhin). Adres avtorov: Mosk-a, 110, 3-ya
Meshchanskaya. u1., d. 6112, Institut eksperimentallnoy patalogii,
i teraDii raka'
(ME;ST NEOPLASMS. etiol' & pathogen.
attempted demonstra;ion-of tumor--oroducing agent
in cancer extracts in mice (Rua))

POGOSYANTS, Ye.Ye.; BOLONINA, N.I.; OLISHEVSKAYA, L.V.
Steppe vole (lagurus lagurus Pall) as a useful new animal for experi-
mental oncological reeenrch. Vop.onk. 5 no.3:281-289 159. (MM 12:12)
1. Institute of Experimental Pathology and Therapy of Cancer, Moscow.
Adree avtora: Moskva, 3-Ya. NeshebaDskaya ul., d. 61/2, Inatitut eks-
perimentallno.v patolog'li i terapii raka.
(NEOPLASMS, exper.
lemming Lagurus lagurus as research animal (Ras))
(LABCRATORY ANIMALS,
lemming Lagtirus lagurus as cancer research animal
(Rua))

BOLONINA, N.I.
Experimental tumors induced in steppe voles with 9,10-dimethyl 1,2-
benzathracene. Vop.onk. 5 no.3:348-351 159. (MIRA 12:12)
1. Iz laboratorii opukholevykh shtammov (zav. - doktor biol.nauk
Te.Te. Pogosyants) otdola etiologii (zav. - deystvitellnyy chlen
ANN SSSR A.D. TimofeyevBkiy) Institute. eksperimentallnoy patologii
i terapii rake, (dir. - chlen-korrespondeni AMN SSSR prof. W.N. Blokhin).
Adres avtora: Moskva, 3-ya Meshchanskaya, d. 61/2, korp.9, Institut
eksperimentalinoy patologii I terapii raka.
(ANTERACENE, rel. cpds.
9,10-dimetbyl 1,2-benzathracene, Induction of exper.
tumors in steppe lemming (Rus))

BOLONUU. N.I.
Tumors inrluced in Lakurus lagurus Pall. by methyleholanthrene.
A transplantable strain of sarcoma in Iagurus. Biul eksp. biol.
i med. 49 no.2:'99-101 F 160. ~MIRA 14.5)
1. Iz laboratc~ii'opukholevvk-h- shtammov (zav. - doktor biologiche-
skikh nauk Ye.Ye.Pogosygnts) otdela etiologii (zav.1- deystvitelInyy
chlen AMN SSSR A.D.TimofpyeVskiy) bstituta eksperimentalinoy
patologil i terapii raka'(dir. - chlen-korrespondent ANN SSSR
N.N.Blokhin) AMN SSSR, Moskva. Predstavlena deystvitelInym chlenom
AMN SSSR A.D.Timofeyevskim.
(TUMORS) (CHOIANTHRENE)

j"i
POGOSYA'NTS, Ye.Ye.; TSUBINA, M.G.;.,BOLONI.NA, N.I.
Selection of hybrid mice for tumor transplantation experiments, Vop.
onk. 10 no.41-53-58 164. (RIHA 17:11)
1. Iz Instituta eksperimentallnoy i klinicheskoy onkologii ANSI SSSR
(dir. - deystvitelinyy chlan At-IN SSSR prof. N.N. Blokhin). Adras avtorov-.
Moak-va, I-110, ulitsa Shchepkina, 61/2, korpus 9, inatitat eksperimentuall-
noy i klinichaskoy onkologii AMSSSR.

PODZEYJ L,Ko;_BOLONlN-A,,.YoI.--.-.- .
Preturaorous changes in the IiVEjr of 057BL mice induced by
orthoftminoazotoluene. Vop. onk. 11 no.12-:94 165.
11)
(MIRA 19.
1. lz patofiziologichaskoy laboratorii (zav. - kand, mod. nauR
I.F. Tereshchanko) Gosudarstvennogo onkologicheskogo in5t!tuta
imeni Gertsena (dlr. - prof. A.N. Novikov).

CHUPEYEV, M.A.; I-I"Klifi NOVA, V.S.; It'l-aOVSKAYA, M.N.; BOLONZIEA. S.S.; IVLEW,
L.D.
Use of surface-active agents in the grinding of carbon black in al-
kyd binding substances. lAkokras. mat. i ikb prim. ne.3:77-78 163.
(14LRA 16:9)
(Paint) (Carbon black) (Surf&ce-active agents)

-PANASYUK, B., meiqdist; BOLONINA, Ye.; MIRMOVA, IOuba (Ryazant)
Uhat are you going to dothis fall? IUn.nat. no.9:16-17 S 160,
(MIIA 140)
1. Pedagogicheskiy kabinet Severo-Kavkazkoy zheleznov dorogi
(for PanaerA). 2. Rukovoditell knithka tovetovodov-krayevoy
stanteii y=atovp Krasnodar (for Bolonina).
(Cities and towns--Civic improvement)

BOLONKIN) A.A. [Bolonkin, 0.0.1
qptimization of parameters in variational problems. Dop. AN URSR
r~-5:580-582 '64* (MIRA 17-6)
Institut kibereatiki AN UkrSSR. Predstavleno akademikom AN Ukr
G.M.Savinym [Saving H.11.1.

--al luc
n V.L ny, I r

Var-1,Ctic,nF~). calcu'lu.,T qri-l f"Ic-IlrAn's fun~~.-..onid ec'- ';Elticn 1, .,he
~nten,-,----ltation of ".1grangr-la llidetendin,te
11 U I""" !! no ~ il' f, 1290-129-", 11,12)
1 7nstitut kil:er-eliki
v
Sav4 rvT. c~v,.r

ACC NRt AT5028934 SOURCE CODE: uR/oooo/65/000/000/0034/oo6,,
1/11, Ss-
AUTHOR: Bolankin. A. A.
ORG: none
TITLE: A method for solving optimal problems
SOURCE: AN UkrSSR. Slazhnyye sistemy upravleniya (Complex control systems). Kiev,
Naukova dumka, 1965, 34-67
TOPIC TAGS: o timum control. pulse regime, particular regime, sliding regime, non-
linear optimum system,
cr+L'A , 0
ABSTRACT: A system descrill~ by,a finite number of ordinary differential equations
is taken for which the optimifm problem is defined as follows: from the set of allow-
able functions y(x), ukx), and parameters c (yW,called the phase coordinates of the
system, is En n-dimensional continuous vector-function defined on the finite interval
whose first derivatives can assume infinite values at a finite number of points;
uW,called the control function,is an r-dimensional vector-function with the same
properties as y(x); and c are constant structural parameters of the system), find
values of YW, il(x), and 6 which minimize a certain performance functional. The
optimum problem formulated in this manner differs from the classical variational prob-
lem: not only the control function u(x), but also the structural parameters are to be
optimized and the study of the optimum problem is.carried out in the class offunctions

L 9731-66
ACC NR: AT5028934 0
whose first derivatives with respect to an independent variable can assume infinite
values. A theorem is proved which establishes sufficient conditions under which the 1
performance functional has an absolute minimum. The method used to prove the theorem
is based on the construction of a so-callect characteristic function T. Three special
modes of operation are investigated: 1) pulsed (discontinuous), 2) particular, and
3) sliding. In the second and third cases, conditions for switching on to such
regimes, operating under such regimes and switching out are established. Two methods
for synthesizing the nonlinear optimum systems are presented. The first method is
based on the construction of an approximate characteristic function and the second
method on the construction of an approximate control function as a function of phase
coordinates and their terminal values. Orig. art. has: 6 figures and 87 formulas.
SUB CODL'-'-: 42 / suBm DATE: o3Aug65/ ORIG REF: 008/ OTH REF: 001/ ATD PRESS:

~BO-WITKIN, A., inzh., orortemen 1-go razryada.
Fundamentals of the theory of flight of rocket models. Kr7l.
rod. 11 no.1:24-25 Ja 160, (MIRA 13-5)
(Rockets-Models)

BOLONKIN, A., inzh., sportsmen I razryada
Dynamic soaring of a model. Kr~vhrod. 13 no.6:24-25
Je 162. (M-LRA 19:1)

BOLAWIN, Alekqandr Aleksaxidrovich; YEFRWIOVA, Ye.V.., red.; IIJAMNOV,
B.B. . r ; OROIET,-A.V., tekhn. red.
(Theory of the flight of flying models]Teoriia poleta le-
taiuslichikh modelei. Moskva, Izd-vo DOSAAF, 1962. 311 P.
(MIRA 15:10)
(Airplanes-Modols) (Aerodynamics)

NATALENKOJ, Valentin Pavlovich, master isporta; YEFREMOVA, Ye.V., red.;
Bglp_44_LN,-A,A.,--.r-ed,L�ORKIN, M.Z., tekhn. red.
(Models flying on cords]Kordovye letaiushchie modeli. Maskyaq
Izd-vo DOSAAF, 1962. 83 P. (MIRA 16:2)
(Airplanes--Models)

BOLONKINY A., inzh., sportsmen 1-go razryada; IEBEDINSKIY, YI.
Victory of Soviet airplane modelists. Kryl.rod. 13
no.11.02-14 N 162. (KTRA 15:12)
(Airplanes-Models)

BDLONKIN, A.
Airplane-model rocket engines. Kryl. rod. 15 no.8: insert 12-15
Ag 164 (MIMA 18:1)

EM (d) #BD/FSS-2/FEC(k) -2/ LJF(c) AST/GS/BG
028935 SOURCE CODE: UR/oO00/65/000/0Oo/oo68/OO90!
AUTHOR: Bolonkin, A. A.
ORG: none
+I
TITLE* Puls~, particularand sliding modes of operation in flight dynamics problems
SOURCE: AN UkrSSR. Slozhnyye sistemy upravleniya (Complex control systems). Kiev,
Naukova. dumka, 1965, 68-90
TOPIC TAGS: automatic control, flight dynamics, sliding regime, pulse regime,
particular regime, AAd6,-.4., a.,A-~otj
4-, - t:
ABS=C"T The tbeory of pulsed, particular, and sliding modes of operation in optimal
systems developed by the author in the same collection of articles (AN UkrSSR.
Slozhnyye sistenrj vpravleniya. Kiev, Naukova dumka, 1965, 34-67) is applied to the
study of the following flight dynamics_ problems: 1) optimization of trajectories of
flight vehicles when the angle of attack and the direction of the thrust vector isl
controlled; 2) optimization of vertical take-off trajectories of an airplane; 3) con-
trolling the thrust of a spacecraft during flight in a central field; 4) the problem
of the maximum flight range of an airplane with a simultaneous optimization of the
wing area. Under certain simplifying assumptions applied to the flight conditions,
the equations of motion are written for all cases, the corresponding variational prob-
lems are formulated, and equations for determining extremals are derived. Analysba
Card

ACC NR:
ACC NR: ATW20935
of puls ed,
Of Pulsed, particular al
were made 1
were made which made * and sliding modes or operation in the above-derined optim
F
it possible in many cases to simplify the solutio
emg. OrIf
lems. OrIg. art. has: 5 figures and 97 formulas. IIKJ
n of these prob.
U CO E.
sB D . I
SUB CODE: BUBO DATE: 03Aug65/ ORIG REP: 0061 OTH REF: 002/ ATD PRESS:
U
CWd 2/2

L 15632-66 EW,T(d)/EWT(I)/LWTfA)Ale(in)/T-2/kW(h)/FCS(k) G3
ACC NR: AT6oO35TO SOURCE CODE- UR/0000/651000/000/0119/0147
'AUTHOR: Bolonkin, A. A.
~ORG: none
TITLE. Investigation of takeoff dynamics of a vertically rising airplane
iSOURCE: Issledovafiiya Po dinamike poleta (Research on flight dynamics), no.'. 1.
!Moscow, Izd-vo Mashinostroyeniye, 1965, lig-i47
TOPIC TAGS: I=- se, VTOL aircraft, vow* --9, vertical takeoff
trajectory, vwl IS =inq~ vertical takeoff **rqawae a-4-c^A0-j
&.141M 41
ABSTRAft: TAe behavkor of a VTOL air2lane during a takeoff maneuver was studied
by means of an 1~-%'electronic analog computerkothe airplane was treated as a
material point, and a system of nondimensional equations of its motion which-
were used in calculation is given; the trajectory was projected on an oscillo-
graph screen so that all stages of the flight and the effects cf all its parameters,
could be easily observed during the investigation. The following problems were
istudied: the takeoff trajectory, velocity, and time for various initial thrust
iangles, at various thrust-to-weight ratios and wing loadings; the effect of the
Cardjlg----, --.-..-.-,,uDc:---629..198.2.005--- --------------

L 15632-66
Acc NR: A%oo457o
langular velocity in tilting the-thrust axis, and of the airplane speed on the
trajectory for various initial thrust angles during the process of switching
~from vertical to horizontal flight; the effect of failure to operate some. It
',engines (so that 25 or 50% of the thrust is lost during the takeoff or when tilting
!,the engines) on the takeoff trajectory. These problems are examined in detail and
are accompanied with a number of diagrams in which the relationships between the
itakeoff parameters and the shapes of the trajectory under various conditions are,
Ishovn. The investigation leads to the conclusion that two patterns of vertical
takeoff are possible: with engines In vertical position, and 'With inclined
engines; both patterns are discussed and illustrated by diagrams. The data
i
obtained can be used as guidelines in studying other problems associated'vith
'vertical takeoff, and will help investigators to obtain answers to them in the
ifirst approximation. The possibility is mentioned of applying the results
lobtained here also to analysis of the vertical takeoff of airplanes equipped
.with tilting reaction engines, or with separate lifting and cruising engines, or
Ivith turboprops. The program of the investigation and of recording the tra-
!jectories is given in an aypendix.. Orig. art. has: 41 figures.. [VKI
MB C OHIO REF: GOV 'ATD PMS:
ODE: MM DATE: 02AUe~/
01P/
!-cut 2 2
a-M 9 WE M R. ~.-

'F
L. 0'469C-67 EW'l d' /EW_1 W) ~Jw
_K X SQURCE CODE: UR/0000/65/C)OO/000/0020/0078
CU-N AT6003568
AUTHOR: Bolonkin, A. A.
ORG: none
TITLE: Optimization of a trajectory of multistage flight vehicle
SOURCE: Issledovaniya po dinamike poleta (Research on Flight dynamics), no. 1.
Moscow, izd-vo Mashinostroyeniye, 1965, 20-78
TOPIC TAGS: spacecraft traject ry, Euler equation, Coriolis force
ABSTRACT: The optimal motion of flight vehicles has been studied by many authors.
However, the majority of these studies were concerned with determining
!.optimal trajectories of single-stage flight vehicles which satisfy only the
first necessary optimality condition-the Euler equations, or the neces-
sary optimality conditions formulated in the form of the maximum principle
of Pontryagin-and were not concerned with other necessary and suffi-
cient optimality conditions.
-In the study reviewed here Ill. A. A. Bolonkin analyzes the optimal
flight of a multistage, flight vehicle in the case when the curvature and the
rotation of the earth are. taken into account and the constraints on the control,
Card
UDC: 629.197-7.005

L C4690-67
ACC NR: AT6003568
functions are expressed by inequalities. All necessary and suificient opti-
mality conditions (the Euler equations, Clebsch, Weierstrass, and Jacobi
conditions) are analyzed on the basis of a general study of necessary and
sufficient optimality conditions in the variational pr-)blem of optimizing
discontinuous control processes with inequality-type constraints imposed
upon the control function presented in the appendix of the article. To
simplify the presentation of the general results, the optimal control is
divided into the following two problems: 1) analysis of necessary and suf-
ficient conditions for the strong relative minimum of the performance func-
tional in the case when the domain in which the control function varies is
bounded, the control function*is discontinuous at certain points, and the
phase trajectory has corner points (so-called discontinuous variational
problem. of the first Idnd); 2) analysis of necessary and sufficient colAtions
for the m'ultistage problem (the discontinuous variational problem of the
becond kind, or the variational problem with discontinuous right-hand sides)
when, in addition to the conditions formulated in the first problem, the
motion of a body is described at various stages by various differential
equations.
The first type of problem is reduced to the ordinary problem of Bolza-
determining the minimum in the class of curves with corner points -and

ACC NR- AT600356s
the second type of problem, to determining the minimum in the class of
curves with corner points which intersectE the given switching surfaces.
The conditions of Euler, Weierstrass, Clebsch, and Jacobi, the Erdman-
Weierstrass corner condition, and the transversality condition, which are
necessary conditions for the normal nonsingular curve (extremal) to mini-
mize the performance functional are analyzed in the discontinuous varia-
1 tional problems of both the first and the second kind. The sufficient con-
ditions of its strong relative minimum are obtained from an analysis of
the second variation of the performance functional. Simple algorithms
for verifying the sufficient conditions are presented.
Since the thrust, mass, aerodynamic, and other characteristics of
the separate stages of p, multistage flight vehicle are different, the problem
of optimizing the flight trajectory is considered as the discontinuous vari-
ational problem of the second kind. The optimal flight problem is analyzed
under the following conditions: 1) the flight vehicle moves in the plane of
a veat circle of the earth; 2) the design of the flight vehicle is known (the
nifraber of stages, the amount of propellant in each stage, and other
parameters); 3) stages separate without shock at the instant that the pro-
pellant is burned out; and 4) the flight vehicle is considered as a mass
point and the earth as a sphere.
Card 3/5

L u4691j-67
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In the orthogonal coordinate system with its origin in the mass point
and the x-axis in the direction of flight, the equation of motion of the vehicle,'
with the curvature of the earth, the components of the Coriolis accelera-
tioh, and the variation of the gravitational acceleration with the altitude
taken into consideration, is set up, using the following simplifying assump-'
tions: 1) the centrifugal force due to rotation of earth is to be neglected;
2) the component of the Coriolis acceleration perpendicular to the plane
of the flight is to be neglected; and 3) the exhaust velocity of combustion
products does not depend on the altitude.
In tile equations of motion, functions L(t), H(t), V(t), 9(t), and m(t)
(flight range, flight altitude, flight velocity, the angle of inclination of the
trajectory with the local horizon, and the mass of the vehicle, respectivel3i
are considered as phase coordinates and functions D(t), w(t), and OW (the
angle of atta'ck, the angle between the thrust vector and the velocity vector,
and the fuel consumption, respectively) as control functions constrained
by certain inequalities. The phase coordinates L(t), H(t), V(t), and 9(t)
are continuous and piecewise differentiable functions, m(t) is a continuous
and piecewise differentiable function in each stage but hhs a finite jump at
the instant the stages separate; control functions c,(t), At), and B-(t~ -have
discontinuities of the first kind.

L G4690-67
ACC NR- AT600568
With the above -formulated conditions, the optimum trajectory of the
flight vehicle is sought from the optimality condition of the given phase
coordinate. The minimum propellant consumption, the maximum terminal
velocity., or others can be taken as the optimizing coordinate. The
boundary conditions at the ends of the trajectory are considered as
fixed, but the case of variable boundary conditions is also analyzed.
In this way, the formulated optimal fligbt problem is considered as the
Mayer variational problem; the results of the general theory presented
in the appendix are applied to its analysis. The necessary and sufficient
conditions for the existence of tile weak and strong relative minima of the
performance functional are verified.
It is concluded that when the Eul~-r conditions and the strengthened
Clebsch and Jacobi conditions are satisfied on a nonsingular curve, this
curve ensures the weak relative minimum of the performance functional,.
and when the Euler and the Weierstrass and Jacobi condi-
tions are satisfied, this curve ensures the strong relative minimum of
the performance. functional. Some peculiarities of the optimal path of a
multistage flight vehicle are presented in connection with the study of
neaessary and srf gien optimality conditions. Orig. art. has: It figurea ands
25 formUa3. v. 2, no*
SUB CQDE: 22p 20 SUBM DATE: 02Aug65 / ORIG REF: Oll / OTH REF: 004
Card rilt; C__

30985
S.1121V6110001-kO09100610.58
D234/W;03
AUMOR: Bolonkin. G.S
TITLE: On the motion of gas in a pipe with movable piston
PERIODICAL: Referativnyy zhurnal. Melchanika, no. 9, 1961, 8,
abstract 9 B44 (Nauch. tr. Mosk. gorn. in-t, 19579
sb. 19, 19-41)
TIXT: The following problem is solved: in an infinite
pipe two pistons with the masses bil and "12 are placed, between them
there is an ideal eras with the mass m and initial parameters F
al . 0 ?0.
At t > 0 the process is regarded as adiabatic, there is no friction
between the pistons and the walls of the pipe, the external pressure
is cqual to 0. The mathematical problem consists in finding the
solution of
32~ /a~~ +1 a2t
aX2 -C2 - 0
0 ~6-x) at2
Card 115

3098.5
S/124/61/000/009/006/058
On the motion of gas... D-2,34/D303
with initial and boundary conditions
k(x ) : a2 14 x 4 al
~011 -
0)
62k -6 where x a
aX2 aj I
JU2 3t where x a
2*
ax Ix
The solution is represented in the form
4(X,t) = 41(t) ~2(x) + U(xlt)
and it is required that
au(.%-,t) _< 1~1(t) ~ ~2(x)
ax
Card 2/5

30985
S/124/61/000/009/006/058
On the motion of gas... D234/D303
~J(t), 42(x) and U(x,t) are determined by expanding them in powers
of a small parameter, which is taken as ~L = ,L-I+ J-,2 -:~ I Z7Abstrac-
ter's note: j~)pears to be a misprint for 1-7 where ill = M41411
2
terms of the order of jj- a-kid higher being discarded.
P2 PI 1121 ca
The functioe ti(t) is found from
0 t
TY
2(x) - x + -6-tZ E(x + a2 )3 3a 2 (x + a 2)2
3a2) (x + a2)]
U(x9t) is represented in the series form
Card 3/5 U(X,t) - Ze Uln(t) U2n(x)

On the motion of gas...
-0985
S 24761/000/009/006/058
D2.4/D303
whereU In (t) t1(t) (rt +1)/4 'k Y-Z' jv (Z) + B V-z YvWj
(x) a (_,),n+l 211-
2n ral + (-I)n,2] sin n (,,, + a
jr3n3 &- T 2)
Here A and B are constant coefficients and
I
Z Rn are sin 4 -157-2
The motion of the pistons for t > kT, the
13-frequency circuit has higher noise (5 times as high in selective reception,
;Z times in homodyne reception) than the Z-frequency regenerative circuit; (4) The
13-frequency circuit has the important advantage of operating with detuned input
I
iwithout impairing its sensitivity. Orig. art. has: 2 figures, 43 formulas, and
I
!I table.
I
;SUB CODE: 09 SUBM DATE: 07Jan65 ORIG REF! 008 OTH REF: 006
!Card 212 hs

1,3!Aa-KOV. BOLOSHIN, T'IRT-XV. D.V.
Pjesikn. cnn-,truction, vnd --tarting cl-Karutions at Ore Tllro3:~Ing Plant-
No.2 of the Krivoy Rog Sout-horn Mming and Clrc- Ttressing Ccmb~~ne.
Ti-adv Makhanobi- no..133:3j~8-3.77 163,
( m I rtk 2 8 : 1c) )

KARPUNIN, P.M.; BOLOTENKO, V.V.
Use of Azotobacter suis culture for swine fattening. Veterinariia,
40 no.70&-59 J1 163. NIRA 16:8)
1. Direktor 14oskovskoy oblastnoy veterinarnoy laboratorii (for
Karpunin). 2. Zaveduy-ushchiy proizvodstvannym otdelom Moskovskoy
oblastnoy veterinarnoy laboratorii (for Bolotenko).
(Azotobacter) (Mciscow Province-Swine-Feeding and feeds)

AUTHORS:
TITLE: Of t~IC- n Over a
1 0
2 2
0:7i
PERIOD'7-C.~-, 2: 1,
(Rer 1 it r; -'iL,-..-n t",.vt the
-.Ctive Z,.rt~clo!~ e atmosi-1:eric
in
:!'I- Vo of to ar
0 In 1 E~ c V. e.,; I t t f -):v :-t -"..:~rc, also
2 2
v r t c- Vl -, 0.-. s
In to the
'aerc C-:-.rrie 7 t ;-,01, -):1 of
c 2 1 1"!
u:-:
t e fa C,2
t'~.u c
c:,,z c,,f t'~.

T
SDI" t If 0
Over
2 2 JU.
Of t"C
ac a
ntc: +
en -
t

Li '1!11 C D
o

if

,
V C -ted fr a in
i
c

C ~he

f;
T
0
f
.
o
.7~rtq
"t in

3" Z; Of t:-,e
0, t'lo Of t'ne
2
e r

f of
O

-
of 0 01-
2 2 ,-
The ;e2
f .
C 0 'ej, T
.t Z; -; f; '
.~! of
- U-
these

The Mechanism of the Vertical Distribution of 11202 30'1/2o-1 2o-1 -31 /063
Ovor a Solution
experiments tend to show the followint;: The decomposition
of the hydro,-:,en peroxide molecules evaporated from the
solution which increases with increasinj; height is connected
with the existence of dust particles in the air. Finally the
authors thank A.N.Frumkin, Member, Acade-ny of Sciences, USSR,
for his mentioning the possibility of the discussed vertical
distribution of H 202' There are 2 fiGures and 7 references,
which are Soviet.
ASSOCIATION: Odesskiy tekhnologicheskiy institut im. I.V. Stalina
(Odessa Technological Institute imeni I.V.Stalin)
PRESENTED: January 2, 1958, by A.N.Prumkin, Member, Academy of
Sciences, USSR
SUBMITTED: November 21, 1957
Card 3/4

The Mechanism of the Vertical Diotribution of 11 0 SOII/ 2o-12o-1--11/63
Over a Solution 2 2
1. Hydrogen peroxide vapors
Card 4/4

S/081/61/000/020/062/oBg
B102/b147
AUTHOR: Bolotioh, 1. P;
TITLE; Investigation of the kinetics of oxide growth on Mg and 11
by optical polarization
PERIODICAL: Referativnyy zhurnal. Khimiya, no. 20, 1961, 264, abstract
201207 (Tr. Odeask. tekhnol. in-ta im. 1. V. Stalina, v. 13,
1960, 21 - 30)
TEXT: The method proposed permits continuous control of the course of the
corrosion process on a metallic surface and does not distort the course of
the process. IAbstraoter's note: Complete translation.
Card 1/1

S/020/61/137/001/018/021
B101/B204
AUTHORS: Roykh, I. L. and Bolotich, I. P.
TITLE: Relation between separated H 0 and the quantity of the
2 2
oxide molecules formed in the atmospheric corrosion of Mg and
Al
PERIODICAL: Doklady Akademii nauk SSSRp v. 137, no. 1, 1961, 126-129
TEXT: It is the purpose of the present paper to prove that the photo-
graphic method of studying the atmospheric corrosion of metals by the
action of the H 0 formed upon the photoemulsion is physically justified.
2 2
For this purpose, a comparison between the results obtained by the
photographic method and those obtained by studying thin oxide films
in polarized light was carried out in the same way as done by P. Drude
(Ref. 3), L. Tronstad, and B, Winterbottom (Ref. 4). For the parameters
,2~ and 4) of the elliptic polarization of light, the Eq. (1) is written
down.
Card 1/ 6

Relation between separated... S/02 61'/137/001/018/021
B101YB204
21P - 2,p rosIT-a
1+
n', A-A a' sin 27,p
A 'Os~'P
n
A LA cos 9 sin' q) (coss (p a) I-XI 2x
Cc o -s$ q)-- a) t -~a,a(I -+xj)j a' 73 (1 + xk)l
L - layer thickness, n refractive index of the layer, wavelength
of the incident monochromatic lig ht, n - refractive index of the metal,
X - absorption coefficient of the metal, y - angle of incidenceoftlibeaml-an-
gle between the oscillation plane of the incident polarized light and the
plane of incidence. In the case of reflection, not only the amplitudes
of the components, bilt also the phases change: 611-6 -,1A.6 and
L
relate to the pure metal surface, A and q to the oxidized surface. For
the optical constants of the pure metal surface it holds that:
- /() + cos-16 sin2T sin-b tan
n - sinytangoos2,1! 2? (2). In order to
Card 2/ 6

Relation between separated... S/020/61/137/00 I A 18/021
B101/B204
create unique reflection conditions, magnesium and aluminum were polished
by means of pastes of the GOI (State Institute of Optics) until the un-
evennesses no longer exceeded 0.14 - 0.1/,L . By means of a polarization-
goniometer constructed by V. A. Marchenko, A and 2i were first determin-
ed, and herefrom n and K were calculated. Next, & ar-6 2~ were determin-
ed in the course of the oxidation process, and herefrom L and n 1were
calculated from (1). ACBA-120A (SVD-120A) lamp, brightness about
5000 stilb, was used for illumination. The following was found with
A = 5890 A: = 600, for aluminum n = 2.37,X = 1.53, n 1= 1.51; for
magnesium n 0.484,)t = 6.93, n1 = 1.7. As shown in Fig. 1, there is
good agreement between the photographic and optical data of the oxidation
kineti cs~.65 or the increase of L, L = 31t was found for aluminum;for mag-
nesium L = 63t was found. The photographic method was checked by
determining the dependence of the density of blackening on the concentra-
tion of H202 vapor. Experiments were carried out at (20+1)OC, the dis-
tance between photographic plate and H202 solution amounted to 2 mm. The
Card 3/6