SCIENTIFIC ABSTRACT PATRAULEA, N. N. - PATRIKEYEV, G. A.

• Document Type: CREST
• Collection: Scientific Abstracts
• Document Number (FOIA) /ESDN (CREST): CIA-RDP86-00513R001239430005-4
• Release Decision: RIF
• Original Classification: S
• Document Page Count: 100
• Document Creation Date: January 3, 2017
• Document Release Date: June 21, 2000
• Sequence Number: 5
• Publication Date: December 31, 1967
• Content Type: SCIENTIFIC ABSTRACT

8D411
Counteracting Tandem Propellers RUK/8-59-1-2/24
1 + f2
. [I + 2V*
1-f2- I + + 97 + 2 V*)
(11-5)
(1 T oo
( 14 o 77 2 +
The quality coefficient is expressed by: 3
I(' + f2) PO* - (fi + f2)]
C = - D- -- -
*2
O'l 11 2 rco + 002
and considering that fl f2 f, the formula (12,1) is changed:
3
3 2f 2
C = (l + f) 1 + f (12.2)
2 1
m + M
Table 1 shows the results of some calculations. It can be observed that
the quality coefficient is greatly influenced by the friction represented
by the coefficient m. The wind tunnel coefficient is expressed by:
Cs . 1 1T4~ + 2V* . 1 +q 0 (13, 1)
Card 8/ 12 ~l ~0 2 + ?,,* 1 + 2 V* /1 012 2

90411
Counteracting Tandem Propellers RUK/8-59-1-2/24
In case that V* - 0, the following expression is obtained for a fix point:
1 + ~o
C (13.2.).
so 2 m
m
The impuls coefficient is computed by introducing J 0, the value of the
total impulses between the two propellers. Thus the Impuls coefficient
is given by: 3 1
(1-f 2 (1+2V*) - 2 + V*
fj
TCO + 2V*)
1 + 2 V* . m + 1 m
At a fixed point the expression becomes-.
3
2
C (14.3)
10 LT *2 1
OD m
Card 9/1.2 Table 2 shows the values of the ratio

'LIOL-11.
Counteracting Tandem Propellers RUM/8-59-1-2/24
C M)
CD
C (1, M)
for different values of the parameters. The impulse coefficient. can be
increased by reducing The coefficient of the aeolian power is
expressed b_v-
I o -I- T-CO
Ce- (l + -2 + 2) 'u. 1 2 To to + 21)
1 (15.4)
2)]
0
with the condition that:
- f,. ( ;rc. + 2) < T 0 TO + 2) ( '40 1 0 (15.5)
If in the presence of a speed at infinite, V, the introduced total power
is zero, the counteracting propeller system Is in a self-rotation region,
This selfrotation coefficient X is expressed by:
fo 1 (l (l fl)) (16-5),
2
Card 10/12 and the traction coefficient CT by:

8DIM.
T_
Counteracting Tandem Propellers R W 8-59-1-2/24
CT - Tro 0 + 2) 1 - fl (TO + 2) (1 + f 2) + 2) (16.8)
1 lleo712 (To +
on the base of the classical theory it is possible to compute the values
which interfere in the mixture phenomenon between a parallel flow with
the speed v and a resting fluid at a great distance from the separation
surface. Fygure 8 shows the variation of the u/vo ratio between the
speed in a point at the y distance from the separation surface and the
nondisturbed speed v . The loss of output has a value of 0.1325. The
author then establisges the equations for p 0 (the coefficient of the
output reduction due to the friction of the flow vein with the external
fluid) and -q 0 (the coefficient of the reduction of the total output of
the vein, due to the mixture with the outer fluid):
Trot LT 1 - 0.0228 1 + 0.00095 L (18.1)
0- rot L L2R
0 - 1 - 0.0571 + 0.00236 2 (18.2)
These evaluations are only estimated, the friction influence depends from
the Reynolds Figure. Counteracting propellers can be used for tne pro-
Card 11/12 duction of a highspeed zone between the 2 propellers. Behind this zone

80~'u
Counteracting Tandem Propellers
RUK/8-59-1-2/24
the kinetic energy of the flow is imposed on the rear propeller and the
stream is being enlarged. The quality coefficient can be improved but
the friction greatly influences this phenomenon, producing a limit for
the quality coefficient, and decreases the more the propellers become ~ciin-~er
acting. An interesting increase has been obtained for the wind turviel and
Impulse coefficients, especially with carefully designed propeller b) ide,3.
The improvement of the other coefficients is not so important. Counter-
acting propellers could be used for a total or partial replacement. elf 'the
wind tunnel diffusers, or for the deflection of a flow produced by the front
propeller, or for the production of a power which is transversal to the flow.
A flow deflection could also be obtained by a non-parallel Instillation of
the propellers.
There are: 9 diagrams, 2 tables, I graph and 6 references, 5 of which Eire
Rumanian and 1 English.
SUBMITTED: October 4. 1958
Card 12/12

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c i i Po~,u I vc to:!ii ne
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Inntitutul de c,,~rdcn
Bucur(Eti, Auna,;l-a
Vol no. 2, 1
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Aoveriiber 191~Q
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Stiintific;:. a -'n;-i erilar si
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Bucim ,:ti, Iiinnia-
Vol. 11, 11 Sept.
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inc 1.

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R/008/60/000/006/005/008
A231/A126
AVrHORS- Patraulea, N.N.; Andrei, ~t.; Rado, Oh.
TITIE: On the aerodynamic calculation of vehicles using the ground affect
MIODICALs Studii 91 oorootTirl do mecApIoR tkplloatA, no. 6, 1960, 1,565 - 1,579
TEXT: The article presents some general considerations on the operation
principle of vehicles based on the ground effect, as well as the aerodynamic Cal-
culation of di*fferent views of the problem, taking into consideration the two
fundamental types, i.e'.. platforms with circular jets and with annular jets. a)
Vehicles in which a potential m6tion is accomplished In the whole space between
the platform and the ground (circular jet): Considered is the hypothetical case
of a vehicle in which an overpressure is achieved under the platform, due to an
irrotational flow of the fluid in the whole space between the platform and the
ground (Fig. 1). Notating with v' the asymptotic velocity and with s the asymp-
totic section after the fluid has been evacuated along the ground supposed to be
perfectly horizontal, the necessary power is that one which corresponds to t~e
kinetic energy far downstream: Nid - j s v'3, (2.1). Considering then that the
jet is not infinitely thin, the stream lines are almost circle arcs, thus the
Card 1/2

P/60/0o/ooo/o~6/005/008
On the aerodynamic calculation of.... A231/A126
hypothesis that the stream lines are-circular can be maintained. The authors
then continue with examining variations of parameters and draw certain conclu-
sions on how the operating characteristics may be improved. There are 8 figures
and 1 non-Soviet-bloc reference. The reference to the English-language publioa-
tion reads: E.K. Liberatore: A parameter for comparing grbund effect vehicles.
Aero-Space-Engineering, October 1959.
SUBMITTED: May 12, 1960
Pigure 1 -
Card 2/2

00 0~27 2~01
AUTHOR: Patraulea, N. N.
30588
VOOV,
KB9/1)3,05
TITLE: Annular wings with jet flaps
V
PERIODICAL: Studii si cercetari de mecanic~C aplicat~" no. 5,
1961, 1675-1060
TEXT: The article deals with the reneral case of the axisymmetri-
cal flow around a jet-flapped annular wing and presents the boun-
dary conditions on the jet-sheet as well as some basic relations
for determining the asymptotic downstream cross-section of the
wake. The tubular jet sheet is characterized by the discharge of
the impulse I, per unity of span and by its initial deflection 9.
3upposing that the speed module in the jet is constant, the impui6e
discharge per unity of transversal len,,th may be expresued by:
pjvj~j
Card 1/6

30588
R/008/61/000/005/034,
Annular wings with jet flaps D289/D305
in which Qi is the total jet discharge and pjvjQ, the total dis-
charge of the impulse module. The total thrust on the W1"1:' IS eT'i"I,
to the initial discharge of the impulse module:
T ~ pjlj,j
and thus, the propulsion power of the pressures on the external
side of the wing will be:
TA ~ Pj'j'j(l - Cos
To determine the asymptotic cross section of' the wake, t)ie :i,~tl-.ir
considers the general case of an annular wing with jet flaps, in
the presence of a permeable surface acting in its interior, suci,
a propeller disk within the wing. The total thrust io given by:
Card 2/6

30588
R/Oos/6i/ooo/oc-, 'oo-- I-)jz:
Annu'~ar wings with jet flaps D289/D305
T ~ I + f So v2
i 0
in which 0"0is the asymptotic cross-section of tI,e v.,ake ~,-.J
velocity within the wake at infinite downstream. J!uwever, T
also be exi~ressed by adding TAto the power a- t ing ,~n t~.c.
element T and to the reactin- power of the je*:
E C,
T = TA+ TW f 1 0
-,'hc-- follov.,ing rel;itioi-.s cLi.,,. ~~e Jeduced fr3m bind
2
f Ijov0= TA4 TE O\
Card -51' 6

30588
R/008/6 1 /000/005/004""o a
Annular wings with jet flaps D289/D305
Considering v 0and the pressure junp~p to be known, then:
TE = S4
Thus, 30 and TA are the only unknown values in (7). Suppc3in6 n--,,...;
that, TA is expressed by
T P- 2
vc~o S f
A 2
in which the dimensionless number,&-is defined by
S 0VO/Sv"
Card 4/ 6

R/0061/000/001')''004, 00t
Armulur wings with jet flaps D269/D305
If the I; rec,-Ure Jump 41,i pcs-1 tive, 4- ~e, 1i t ractive ~ i-
~3ed, then
v ", v
i.e. the jet tube expands due to tl-,e -i-tlon )f u prisjlve
surface. The author finally examines t,.e ,--irlation of
,i~:n around the annular .,,ing in case o' finite and
L
3- -roqs section. There are 3 fi,-ures --.nd Soviet-Ll, e e: r-:~
'~T!BMITTED,- June 10, !?~l
C,i - d 6 'E

PAiw~;Jik- -
Three-dimensio-n' rheoelectric nnalng~ without the influence of
the bourdarles. Studii cerc mcc apl 12 -c.6:1187-1191 '62.

349'L2
L k.,
t i L;
-0 c t s C) ~3 u
L
I c d v e n --o
%r
u r u ..u C'I.. I f "CU
:3,. 0 ca .48 C. L;'c,, ~;c j J,..,L!I,
e ex-
-ard 1/2

04880-07 I'INT (Ill)/ 11N (k) 4-Arp (w) /nt I,(%,) FN
ACC NRt AP6025065 SOURCE CODE: HU/0019/66/011/002/0341,10351
AUTHOR: Patraulea, N.N.
ORG: Institute of Fluld Mechanics, Academy of the Scw!.-d1st Republic of Rumania, BuchareEA
(Instltdit -deAfec-an1q-u-o do- F-lu-Ides do
TrFLE: Calculation of the jet flap controlled lifting propeller
SOURCE: Revue Rournaine des sciences tee',miques. Serte de mecanique applIquee, v. 11, no.
2, 1966, 341-351
TOPIC TAGS- helicopter rotor, jet vane, lift coefficient, thrust control
ABSTRACT: A theory is developed of jet, flap controlled liellcoptor rotors which are powered
not only by the jet flap's but also by some other (niechanical or pnetunntic) means. It is assumed
that the jet flaps are fixed to the outer half of the rotor blades. Graphs are plotted which show
the ratio IL L11 2 x ,0"291 (o. - 2n(x0)2jZ + 4,7 (c, -27rao) + 1918W between the
+ 2o.
3w
moment produced by the jet flaps and the total moment, as a function of the angle of attack of
UDC: 532

L 04880-67
ACC NR1 AP6025065 4~
the blades a*, the lift coefficient cz, and 7), a parameter associated with the Induced axial
velocity in the plane of the rotor disc. In terms of power, the graphs indicate that it Is efficient
to have a large mechanical factor of the rotor driving force, which corresponds to small values
of P - The transverse curve In each graph represents the lower applicability bound of the graphs.
'Below this curve, jet flap control is no longer feasible, and a more precise analysis of control-~
lability Is required. OrIg. art. has: 6 figures and 26 formulas.
SUB CODE: 01/ SUBM DATE: 05Nov65

-WP(m)/EPR/FCS(k)/EdA(l) Pd-I/PI-4 Wei
L 54056-65 EWT(I)/z
ION-NR.,- -AP4049972- R/0119164/009/005/0999/1003-- -
AUTHOR: Patraulea,- N. N. (CorresPonding member MM)
TME:. An approximate solution withapparent velocity profiles for the'equations
of'the boundaU layer with suction or blowing applied at the wall
SOURCE: Revue Roumaine des sciences techniques. Serie de mecanique appliaueep
'j. 9, no..5, 1964, 999-1003
TOPIC TAGS: boundary layer, velocity profile, laminar flow, hydromechanics
As reported in previous publications, the~equations of the laninar
ABSTRACT.,
boundary layer with suction or blowing applied at the wall,-and in the absence of
a pressure gradient, permit the following simple solutioa.,-
ev
Y - f M,
is-the velocity normal to the wall (V / 0 in the case of suction and
where Vo 0
V >-O in the case of blowina), y is the ordinate, u - velocity in the boundary
0
layer, V - velocity of the external current, and V is thc coefficient of ;-incm-tic
viscosity. Starting from the above con r, iderat ions, the author has previously
shown thae in the case of linear diffusion, applied to-the study of tbe bouneary
L!;?rd 1/2

ACCESSION NR* AP4049972
-e case
solutions with velocity profiles similar to those encountered in th
of a non-uniform exteraal current may be found* The purpose of-the present In-
vestigation was to dateiviine whether the rigorous equations of the incompres!iiblo
boundary layer would also permit such a solution. In the final analysl:q,
it was found that a rigorous solution of the proposed problem does not exist.
Subsequently, the author explains the technique of finding an apparent solution,
if certain approximations are introduced and accepted. The author states that
the approximate solutions obtained in the present investigation are "closer to
reality" than those reported in previous articles. Orig. art. has: 31 forxulas.
A5S0C,=10H:_ -None-,
SUBMT=D: 13Hay54 -ENCL: 00 SUB GODE: ME
90 _RBF SOV: .000 UTHER% 003
V2

FATRAJUA., N.N,
Approxim,ite witti profilezi of aimllrir !3p--,3,1 ,' -'he
equations of boandary Inyor with suction or
continuous blowing, Studli cerc mac apl 17 no.5il.'71-12'15
164.
1. 117'raian Vu-q" InstItute r~f Applied 1,~- -.I- Rar"'ar-ar
Academy, Buchare5ti CorrespondtnR Member cr t.he 7~ima:~-,ar
SubT.Itted May 11, 296".
. I

16 15,
28.

PATRAULEA N.N.
-
Extension of the Mestcherski relativistic equation. Rev
mee appi 9 no. 31569-530 164.

PATRAULLA, N,N.
Simi , ar so-~u,-ona of Via diffusion equation to the
laminar boundary layer with auction and blowing. Rev mec appi
9 no.4i819-826 164.
1. Corresponding Mamber of the Awnanian Academy.
V '.P

PATRAULEA, U.N.
On the relativistic extension of Mescerskis equation.
Studil cere mec apl 15 no.1t5_16 164.
1. Corresponding member of the FUcanian Acadeny.

R/0006/64/015/001/0005/0016
ACMSION NR: AP40401"
AUTHOR: Patraulea, N. N. (Corresponding member)
T*ITLE: The relativistic extension of Mexcerski's equation
SOURCE: Studii Bi carcetari de mecanica aplicata, v. 13, no. 1, 1964, 5-16
TOPIC TAGS: Moscerski's equation,'variable mass, relativity, light, velocity,
rocket, propellant ejection, velocity qxuidrivector, inertial reference system,
acceleration, random cosmic particle, photomic rocket, cosmic resistance, collision)
propellant consumption, trajectory, matrix, direction change
:ABSTRACT: The present work is concerned with the extension of Mescerski's equation
about the motion of a material point having a variable mass to the velocity of a
Irocket close to the speed of light, and to some relativistic ejection speeds of
V
1propollant. TI-a motion with respect to an inertial system coinciding with the
imovl--i '~ material point (the rocket) is first determined followed by the goneraliza-
tion to aW inertial reference system. The following topics are theoretically
icovered: velocity and acceleration of the rocket propellant ejection, cosmic resis-'
Itance due to collision with random cosmic particles, propel2ant consumption needed
LC;Rrd 1/~

FW,;OA(b)/17JT(d)/FAA/ZWT(M)/ BDS--AEDYAFn MW/APGG7Fd-4/Pe-4
T%ASD~
1,211"3 ~YAWVYBOOKEX LOIT TI N R~xI6236
Patraulea H. N..
S~udii de aerodinamica hiperzustentaliel; zbcoiul au decolare I
ater*izare scurtwa sau la verticaltY (Study tm Aerodynamics Of
Hypersustentation; Short and Vertical Talvoflr^ and Landing)
[BuchareatI.Ed. AcademieiRPR., 1962. 62!i P. 75D copies printed.
Reap. Zd.-j Dilcu Boice;dQu,; Tech.-Ed.: Petru Bruml.
PURPOSE3 This book.19 intended for researchers and engineers In
aeronautics and related.fields.
COVMUM ~The problem a"as and theorv of V/STOL are explored.
Discussed are hypersustentation (I-e-j *_pTr=_E lift -systems) and
Ipertinent designs and devices, such as bowndary-layer and aerody'.
namic-eirculation control devices; permeable, nonpermeable,, and
jet flaps; toroidal., annular, and annular jet winZB3 fl7ing plat-
forma~(Zround-effect and air-tushlon)j and deflected-jit, Blown-wing
Card 1/1)
11115 ~R-Wl

0 RUM/6236
j2w,_6 Rnd autargiro-type aircraft. An examination of'wrheoelectric
analoS7 :.s Included. The author) a contributor on aeronautics
to-Beien4v64flc.pablioation-o,,olaits some ideas In this book as
'his own or as,those of.Rumanian scientists. No personalities
are mentionPd. Re," renceB accompany each chapter.
TA= OF CONTMSi
Ch.- I* General Examination, of Shorb and Vertical, Takeoffs
-sbd Landin (STOL and VTOL)
1..Utility of INSTOL ~6ircraft
2. General examination of-lift
Claabification of'Y/STOL 41iraraft 21
asnificati~6n,of hypertuatentation dev on:
Cl io
Ior4ircraft wings 33
"A f
iciency of hypersustentation.deviceis 3
References,
4h. IL General Principles of Mathematical Determination
of the Notion of a Fluid. Theory of'Rheoelectric Analogy
.1. General mathematics 39
C ard 2/4
WIMM IT

PHASE I BOOK EXPLOITATION RUM/6236
Patraulea, N. N.
Studit de aerodinamica hipersustentatiet; zborul cu decolare pi
aterizare scurta' sau la verticaliT (Study on Aerodynamics or
Hypersustentation; Short and Vertical Takeoff and Landing)
[Bucharest] Ed. Academiel RPH, 1962. 625 P. 750 copies printed.
Resp. Ed.: Dlicu BoIcesau; Tech. Ed.: Petru Brumi.
PURPOSE: This book is Intended for researchers and engineers In
aeronautics and related fields.
COVERAGE: The problem areas and theory of V/STOL are explored.
Discussed are hypersustentation (i.e., optimam lift systems) and
pertinent designs and devices, such as boundary-layer and aerody-
namic-circulation control devices; permeable, nonpermeable, and
jet flaps; toroidal, annular, and annular jet wings; flying plat-
forms (ground-effect and air-cushion); and deflected-jet, blown-wing
Card 1/14

and autcigiro-type aircraft. An examination of a rbeoelectric
analogy is included. The author, a contributor on aeronautics
to scientific publications,claims some ideas in this book as
his own or as those of Rumanian scientists. No personalities
are mentioned. References accompany each chapter.
TABLE OF CONTENTS.
Ch. I. General Examination of Short and Vertical Takeoffs
and Landings (STOL and VTOL)
1. Utility of V/STOL aircraft
2. General examination of lift
3. Classification of V/STOL Wircraft
4. Classification of hypersustentation devices
for aircraft wings
Efficiency of hypersustentation devices
References
2
13
14
21
33
35
36
Ch. II. General Principles of Mathematical Determination
of the Motion of a Fluid. Theory of Rheoelectric Analogy
1. General mathematics 39
Card 2/14

13c: id nr of' th n-vm I! (-d rr ~-s In
cn Tiia iiepuhlicii Pupuhrr :tunir-c.
j~F, IJECA
Instit~itul de Mr~cr~nica A:-Jicata)
Buc,,ircsti , Rumania
Vol. 4, no. 3, 1~~ 9.
Monthl,k list of Lastern I'uropran Acce.-r- ot In-ex (~-FIAI) Lc. ,,nl.
November 195~,,
Uncl.

PAnEWAO V.A.
Panctioma disorders of extemal reepiW.Ion azd their migzifi-
cuts Sm the evaluatIM the vork capacity of patients vith mml-
festatime of cormary lwmfficieneye Terapoarkh, 32 mo,D23-27
Ja 160* (KM 13110)
(WRONAET DISUBS) (MWIRATION)
(MBABILITr NAMATION)
I.'I

PATREYEVA, V. A. Cand Med bei -- (diss) "Disturbance of exterzxl respiration
in *z*ws=&:P coronary Oiioiency and its importance for the establishment of
work fitness*" Gorlkiy. 1959. 12 pp (Gortkiy State Med Inst im t. M. Kirov),
200 copies (KL, 47-59, 117)
-51-

PATRICIII. El.
S Given Names
Countx7s Rumarda
Aca~amic Degrees% -Researcher; Corootor-
Affiliations Meteorolosioal Institute (Institutul Meteorologic).
t~ ----------
Scarcox Bucharest, Stlinta si Tehnica, No 9, Sep 19619 pp 16-17.
Was "The Automatic Rumanian Meteorological Station.0
IFO

PATRICHA, G.K., inzh.
Stationary lighting of man-engines. Betop. truda v prom. ) no.11:37
N 159. (MIRA 13:3)
I.Shakhta No.32 tresta Snezhnyanantratsit.
(van-engines)

PATRICHF, C.,, ing.
---
Graphic method for processing the central seismosouncIngs. Rev min
14 no-1:39-41 Ja 163.

FATRICIU,jj.
The Resita Metallurgical Plant contributes to the intense industriali-
zation of Rumania. p. 683
MF,TALURGIA SI CCNSTRUCTIA DR KASINI. (Ministerul Industriei Ketalurgice
ei Constructi1lor do Masins si Asociatia Stiintifica a Inginerilor 91
Toobnicienilor din Rominia) Bucuresti, Rumania
Vol, 11, no, 8p Augg 1959
Monthly I49t of East European Accessions (EEAI) IZ Vol. 9, no 2 Feb. 195&.
Uncl.

-- -J~~~-42mriciuq V. ] (R*Yniya)
How to eotablJob holiotl*rjw, Vop, kurot fizioter. i lech. fiz,
kullt. 26 no. 2sI60-164 Px-Ap 161. (MIM 14:4)
(HDROTMOT)

PATt-dClU., V., prof.
"Geology of coal dcpo.~It,~ particularly in Rumnia" by Gr.iiaileanu,
N.Grigoras, N.Onco3cu. Reviewed by V.Patriciu. Rev min 15 no.3:152
Vw '64,

FATPICIU, V.
Geologic studies in the region )f Surducul ~fjaro- P. "5?.
AN ALIL3 SERIA STISTLLOR I?ATJUlI. Bucureuti, Rumania. Vol. 7, no. 195Fj.
Sent.
14onthl.,., List of FaE:t luropean Accessions (EF-AI), LO. Vol. 5, no. 9,/19r9.
Uncl.

PATRICIU . V. 2-,
"J~7drogeological drtlling" by (I.Costacho. Revimmd by
V.Patriciu. Rev min 14 no.121568 D'63.

PA7RICIU, Valerlu, prof. Ar. 1290
How to construct artificial heliothermal lakes. Meteorologia
hidrol gosp 7 no.2t83-90 162.

PATRIE 1. kand.sellskokhozyaystvenhykh nauk; PREVO, A... kand.
-'Z:~~icheskikh nauk
Increased efficiency in poultry procurement and fattening.
Mias. ind. SSSR 31 no.4:36-38 160. (MIM 14:71
1. TSentrallnyy nauchno-issledovatellskiy institut ptitseperera-
batyvayushchey promyshlennostio
(Poultry industry)

PA7RIMEVAV N.A. p zasluzhemVy uchitel I sbkoly RSFSR
Model of a remote control system. Fis, v dbkole 20 no.6:66-67
W-D 160, (MIRA 14:2)
1* 97-7a sbkolap Moskva.
(Remote control)

PATIPJKJI A. :11.
Surgeons
ole of V. A. Ratiimov in the development of Russian Surgery. Vest, Khir. 72,
I
R
No. 2., 1952.
9. Monthly List of Russian Accessions, Library of Congress, Aw,ust -1958. Unclassified.

;"A'.1als -- P ~-Iltry Q
'Ls J. ir Rcf z ur - Bi )1. , t; 1~, lqr~8, 69414
A~:t.. r Patrik I.A.
List
Title Effect -,f S': t..C Or._--i,,isl.-. -,I' HL. ~s
OrI ~~ Pib Pt I t sev x1!3tv 3-1-35
Abstract TI., f 4c f JC4r-04 daily, Pr-~'- '~e-lcl t -1
vari s.Ly c-~;ip -od mti , sli ;htly i. cr,-:~,.sed t'-.,~
pr 1 cti f (tY 3-0-il'), C t weii-lit
s -st 53 i th L' C -tr 1~', a.',d c!~ick hatcl,!
(L'Y 11.8-3.65,). i.. V. e expcrLic.itai ;I' LIP5, tl;u H1- c~-;.-
t C', 't i:'. the U cl 'A 1~e- a~A :i Iting was lul-lyud.
It is roc .!,.,e:.dcd t c -tr)l r7iti)ns ,f heiis wit!-. re-
n -(~ t A, -ti-t -.-. ti.L b-i~~is --f I", ::,.- per 13C : f
dry F.M. K%z-,..-ts,%'
car's 1/1

PATRIK I A kand. sellskokhoz. nauk; VINOGRADOVA, A.P., kand.
.1 010
Be! Uokhoz. nauk; YERMOLffEVA, A.L., mladshiy nauchnyy sotrudnik
Raining meat chicken in cagen. Trudy T.1,NI1PFa 9146-53 '62.
(MIRA 16:6)
(Poultry industry)

BOGOLYUB3KIY, S.I.; VASIL'YEV, V.G.; IOTSYUS, G.F., kand. sell-
khoz. nauk; KO11DRATYUK, N.D., karid. ekon. nauk; FATIPIX,
1,6., kand. sellkhoz. nauk; PELITSM, S.O., kand. sell;;
khoz. nauk; OZMNEV, S.I., akademik; TIKHOMIROV, A.Ye.,,
kand. tekhn. nauk; FEDOROVSKIY, N.P., kand. biol. nauk;
GROMOVA, A.V., red,
(Manual for the poultry farmer) Spravochnik ptitsevoda.
Izd.2., perer. i dop. Moskva, Kolos, 1965. 413 p.
(MIRA 18t7)
1. Vsesoyuznaya akademiya sellskokhozyaystvennykh nauk
ienni V.I.Lenina (for Smetnev).

PATRIKv I.A. kand. sellskokhoz. nauk; PREVO, A.A., kand. biol. nauk
App3yIng more efficient methode for duckling fattening Trudy
TSNIIPPa 9t53-60 162. (MM 16;6)
(DuckB-FeedinR and feedB)

PATRIK I.A. kand. seliskokhoz. nau1c; LAZAREV, Ye.F., starBhiy nauchnyy
...ZiNiva-
bullru
Animal fats and their use in poultry fattening Trudy TSNIIPPa
9:60-70 162. NIRA 16:6)
(Pbultry~--Feeding and feeds)

PATRIKO I A kand. seltakokhoz. nauk
I
Use of phosphatides in the growing of meat chicken (broilers).
Trudy TSNnppa 9t70.74 162, (MIRA 16W
(Poultry-Feeding and foods)
(PhosphatideB)

ARSENSHVILI, A.Yu.; BOGDANOV, M.N.; GORIZONTOVA, Ye.A.; YERSBOVA, Ye.I.;
YEIMBAU,:, N.I.; IOFE, N.Sh.; KARAVAYEV, A.M.;KOLOBOV, G.M.;
LOBIN, N.V., kand. sellkhoz. nauk; YMSEMEER, Kh.F., dokt,)r bilog.
nauk; MISM, P.N.;---LA-TRU-,-1.A.,.-kand. sellkhoz. nauk; RMIPM,
V.K., kane. sellkhoz. nauk.; SENTNEV, S.I., akademik; MAOLETOV,
A.I.; FILASOV, V.V.; SHKUDOVA, R.I.; SOKOWVA, G.S., red.;
ROMOVICH, Ye.F., red.; LEVDA, L.G., tek-hn. red.
[Chickens for meat] TSypliata na miaso. Moskva, Izd-vo 1-1-va
sell.khoz. "LSFSR, 1960. 197 p. NIRA 15 -- 1)
(Poultry)

PATRIK, I. A.
"The Effect of PhosDhatides on Chick Growth and on
the Chemical Content of their Meat"
Report submitted for the Twelfth World's Poultry Congress,
Sydney, Australia 10-18 Aug 1962

PATHIK, I.A., kand. sel'skokho2. nauk
Raising ducklings for meat production. Ptitg&vDdBtvO 9 nO-4--16-20
AP '59. (MIRA 12:6)
(Ducks)

VOLKOV, V.A.; FICDOROVSXIY. kand.biolog.nniik; PZNIONZWVICH. N.B.,
prof., doktor biolog.nouk; RASLIYICV, I.T.. kand.sellskokhoz.nauk;
KRIM, A.A., kBnd. eel I skolchoz.wak;-TATRIK, I.A., kand.sellskokhoz.
neuk; KALINOVSKAYA, A.S., kand.biolog.ii,~ui; DAMOV:11Y. N.V.,
Vmnd.blolog.nBuk; ORWV, K.V., kand.sel'skokhot.nauk; REDW, V.K..
kand.sellskokhoz.nouk; GOFKAN, M.B., zootekhnik; GRIGORIYEV. G.K..
stershiy nauchnyy sotrudnik; GORIZONTOVA, Ye.A., starshiy nauchnyy
sotrudnik; FEOKTISTOV, P.I., kand.veter.nauk; KOTELINIKOV, G.A.,
kand.veterin.nauk; SMaWYA, R.I., red.; BALAKIN, V.M., red.;
GRADUSOV. Yu.N.. red.; SOKOLOVA, G.S.. red.; SAYTANIDI, L.D.,
tekhn.red.
[Dack raising] UtkovodBtVO. Izd-vo H-va sellkhoz. R.S.F.S.R.,
1959. 284 p. (MIRA 13:12)
1. Nachallnik Glavnogo upravloniya ptitsevodstva Hinister8tva
sel'skogo kh02yayBtVB RSFSR (for Volkov). 2. Vaesoyuznyy nauchno-
iseledovateltakiy institut ptitsepromyshlennosti (for Grigorlyav).
3. TSentrallnyy nauchnowifieledovatelJ-skiy institnt ptitseperera-
botyvayushchey promyshlennosti (for Gorizontovb).
(Ducks)

SCiMBNOVICH. V.B.
'Intestinal protozoal diseases in can'. N.A. Patrik. Reviewed by
V.B. SchenBnovich. Hed. paraz. 25 no.lt88 i9tWI5 (MLRA 9.6)
(INTESTINES-DISBASNS) (PROTOZOA, PATHOGENIC)
(PATRIK, N.A.)

pmu.' N. P.
OIntestinal Hemorrhage in Gases of Kxanthematous Typhus,* Klin. sad., 26, No.6,
1946
Clinic Infectious Disewesp Kazakh State Mod. Inst,. in. Molotov

'-; A'--'---L " . I . . . .
2 , -.- ~, , ::. i . , , , -, r ~ -'. ! -': ~ . -~ :-. a .' , -,,~ ~ :,-' ~ - a :,. ~, ' :-, - - -!I., - " *- ---I., - - - .
ZI-lra-,7oo'-!-.r,-~-i--.---* -,-.: I I I.,- -. - I'll -
, - --, -, ." , - 1, - . -, - --,.
j r : T -.~ ,-~ ~` . . - I
- - , 2 ~~ , . ' . --,,.

PATRII, N. V.
I W. f-~
`1111~,=Q9-6 fiil baleatidiasis and its treatment with osarsol. Truly Inst.
kraev. pat. AN Kazakh.SSR 1:5-9 152. (MW 10:2)
(AWTARONES) (BAIANTIDM COLI)

PATRI11K, N. P.
i3alantidium Ooli
Intestinal balantidiasis and its treatiatnt. Klin. iried. 30, no. 2, ~et). 1)52
L
9. Monthl List of Russian Accessions, Library of Congress, AL-7ust - 195,~, Uncl.

MARGOLINA, L.
"Protozoal intestinal diseases in manO by U.P.Patrik. Reviewed by
L.Kargalins. Imb.delo 3 no.4:59-60 J1-Ag 157. (MMA 10%8)
(INUSTIBES-DISEASES) (PROTOZOA, PATHOGENIC)
(PATRIX, N.P.)
MISIMM,MHOW

FATRIK, N.P., prof.; ZJCYTLENOK. M.A., doteent
"Course on infectious diocases" by A.F.Billbin, K-V-Bunin.
Reviewed by N.P.Patrik, M.A.Zeitlenok. Sov.med. 21 no.8:150-152
Ag '57. (MIRA 10:12)
(CCRMUNICABLIC DISEASES) (BILIBIN, A.F.) (BUNIN, K.V.)

PATRIK, N.P., prof.
Review of V.P. PbdItapollskaia. and V.P. Kapustin's book wHelminth
diseases of man." Sov.med. 23 no.9:110-150 S 159. (MIRA 11:1)
(WORMS, INESTDIAL AND PARASITIC)
(PODIIIAPOLISKAIA, V.P.) (KAFUSTIV, V.F.)

FATHIN, B., 1nz1h.
Tiling roofs. Sell. strot. 9 no-5:20-22 Ag '54. (MIRA 13:2)
(Tiles, Roofing)

PATRIK, S. [Patryk, S.], in2h.
Covering roof slopes with ribbed slag-cement sheets. Sil'.brud.
7 n0-7:8-10 Jl '57. (MIRA 12:11)
(Roofing, Concrete)
PIV

PATRIK, S., inzhener.
-
Rolling and storing clay as a method of improving the quality of
bricks. Stroi.mat. 3 no.8:19-21 Ag '57. (MMIA 10;10)
(Brickmaking)

PATRM,_,&,A.; ISHEUNOV, G.S.. nBuchnyy red.; KOVSHOVA, O.W., redo;
JIPOOI~DVA, M.F,, takhn.rad.
[Tiled roofs] CherepichnBis krovlia. Moskva. 1958. 127 p.
(Tiles. Roofing)

GAK? B.N., kand.tekhn. nauk; GERVIDS, I.A., kand. tekhn. nauk; G~;NCHAR,
P.D., lnzh.; VASILIKOV, S.G., kand. tekhn. nauk; YEVNEVICH, AA,
kAnd. tekhn.nauk; XIPTENKO, A.Y., lnzh.; LUNDINA, M.G., kand.
tekhn.nauk; NAUWV, MA, kAno. tekhn. naukj PAj'RJX,_,,'1P ', A~ , irjzh. I
POPOV L.N.V P inz- .;
I kand. tekhn. nauk; !t,C0VDY, MI.I."" h SEW V, V. G. ,
lnzh.; SOKOLOV, Yu.B., inzh.; FRANCHUK, K.O., lnzh.; KHAYKIN,
V.Ya., inzh., nauchnyy red.; CHIBUNDVSKIY, N.G., inzh., nauchnyy
red.; NOXHRATYAN, X.A., red. [deceased]; GUZMAN, M.A., red.
DURVICHO E.A., red.; BO&WIEV, N.K., tokhn. rod.
[Handbook on the production of structural ceramics)Spravochnik
po, proizvodstvu stroitellnoi kerwdki. Moskva, Gosstroiizdat.
Vol.3.[Wall and roofing ceramics)Stenovaia i krovellnaia kera-
mika. Pod red. M.T'.Nairnova i K.A.Nokhratiana. 1962. 699 p.
(MIRA 16:1)
(Ceramics) (Building materials industry)

PATRIK,_B-Lv-r-4rszh.
Expansion of roof-tile production. Stroi. mat. 5 no.5:4-6 -
MY 159. (141.U 12 - $)
(Tiles, Roofing)

PATRIX, S.A.
(Mining and storing clay under winter conditions] DoIjycha I
khranente gliny v zimnikh usloviiakh. Kcskva. Promstroiftdat.
1954. 144 p. (KM 7:11D)

PATRIK, N. P., Prof.
PA 14/49T63
inn
Medicine Nrwrrhage
"Intestinal Hemorrhage In Cases of Rranthematoue
Typhus,* Prof IV. F. Patrik and B. Kadyrova, Clinic
of Infectious Diseases Khrakhok State Med Inst
imed V. M. Molotorp 4 YP
"Klin Mod" Vol =I, no 6
Contrary to accepted Ideas, Intestinal hemorrhage Is
riot rare typhus complication. Prognosis Is, as a
rule, favorable. Pathogenesis Is complicated.
Hemorrhagic forms of typhol&-aasily mistaken for
those of typhus.
ANM3

PATIN, H.P.
Intestinal balantidisels and its therapy. Klin. med., )4o$kva 30 ao.2:
44-47 Fob 1952. (MAL 22: 1)
1. Of the Institute of Andemic Pathology of the Acadergy of Scierces
Kazakh SSR (Bead of laboratory of Medical Parasitology -- Honored
Worker in Saienas Prof. 1. P. Fatrik). Alma-Ata.

PATRIK, S.A., inzhener.
------- __ -
gechanized clay supplying of the brick industry in cold weather conditions.
Mekh.stroi. 10 no.7.*20-27 JI 151. (mlu 6: 7 )
(Brick industry--Gold weather operations)

.1 1 -/. I
UIVII. Roman Yefimovich; professor. dolctor tekbuigheakikh nauk; KRUGLYT. S.M.,
redaktor; PATRIKI T* X.. redaktor iz"tell stys.; BZRWV, AP., tokhnicheskiy
rodaktor*
(low evaporstore)Vo-wri vyparnol appar&%. Moskva, Gon.nauchno-tekhn.
isd-yo lit-ry po chernoi i tayetnot mot4llurgii, 1957. 199 Pe
(MLPA 10-- 5 )
(3vaporating apAU%fts)

Kh.M.; PATid&6ViGh, S.B.; )a--SIUUYAZUVA, N.
Determining the tcxigenicity of diphtheria bacte.-ia by the diffusion
method in mixed and pure cultures. Med. zhur. UzI)- no-3:69-71 Mr 160.
(1'1"1 15:2)
1. Iz kafedry mik-roblolo,,ji (zav. - prof. P.F.Samvonov) Tashkantakogo
gosudarstvennogo madit5inskogo inotituta.
(~;OI-*-:,ACT-i-dLW, DINITH&i-dA.:-~)

1 . VER"'INSOONOV, V.YA. ; PATRIX'EY, N.M.
2. USSI~ (600)
4. Windbreaks, Shelterbelts, Etc.
7. Renew and extend shelterbelts according to plan. Les.1 step' 4 no.10, 1952.
9. MonthIj List of Russian Accessions, Library of Congress, ~anu&= -1953. Unclassified.1

r,) r,: ~: t
A~
,)I) C C c'SS '~!S rji
9. Monibly List of Russian Accessions, Library of Congress, hpr-195~, Uncl.

PATRIDYXV, A.
ShT 11-150 swivel. Nsv.neft.tekh.:Bar.n*.7:3 '48. (KLRA 9:4)
(Oil well drillizE-Squipment and supplies)

PATRInYNV, A.
Organizing competition among drivers In Omsk. Ayt.tranap-33
no.10:37 0 '55- (MM 9:1)
(Omsk--Kotorbus c1rivers)

PATRIKEYEV, A.B., I n 7_h . ~ S RC j!j p Y,-,.A., Inzh.
Horizontal force interaction of running wheels c~~
cranes. Vest. mashinostr. 45 no.1~31-34 Ja 165.
f M ;-.1 11 ;~ " ~'

PATRIKEYMT, -A.-B.., i-nzh
Side forces of runrinF wheels of ground-type charging mac* ,'Lnes.
Vest. mashinostr. 45 no. 12:3q-41 D 165 (,TRA 19:1)

124-57-2-253"1
Translation from: Referativnyy zhurrial, Meklianika, 1957, Nr Z, p 14 1 (USSR)
AUTHORS- Patrikeyev, A. V. Chibrikin, M. V.
'rITLE: On Fatigue Testing of Wood (K VOPI-OSU ob issledov.%nii drevesiny
na ustalost' )
PERIODICAL: V sb. : Vopr. drevesinovedeniya. M -scow- Leningrad,
Goslcsbumizdat, 1953, pp 64-71
ABSTRACT: A testing technique is propounded for fatigue testing of wood
(the shape of a specimen- and a fastening method therefor, the
number of stress cycles per minute, the maximal number of
cycles, a schematic design for a testing machine, etc. ) The
fatigue limits found in the investigation of pine and beech amounted
to 22-251/o of the ultimate static strength for static tangential
flexure.
2. ".)od-l'ost Meth(Af; A. F. Rozhnyato%,,skLy
Card 1/1

PATRIKEYLV, B.; INSHENETSKA, V.
1.
2.
(for
hoproving the asbambly of large-panel building&. Ila Btroi. hoo. 3 no.3:
1
11-10 Rr W. O'll'u, I i,:, )
Glavnyy inzh. upravleniya Sverd1ovskg-v-1tr,-.y (for Patrikeyev,).
Nachaltnik tekhnicheakogo otdela upra-vieni.ya 6verdlovskgorstroya
Imshenutskiy).
(Sverdkovsk,--Apartmont IIOLISOS)(Precast concrete cowtructiou)

Dintrz lX2c(l)
-Y
rT
-afa o~t-IL'll
Mil..
in f1b,")b
A" I
GT4 IT

BURGHB, Te.F. , voyaninshener 3 ranga; VLADIHIROV, N.A.; TEPLI16KIY, B.L.,
general-mayor avistsli, redaktor; PATRIKEYEV, F.A., mayor, redaktni-;
DOZHDIV, I.M.. tekhnicheekly redakCo-r"-----
(Military aircraft of the U.S.S.R.] Voennys samolety SSSR. Mosk7a,
Voennoe izd-vo fiarodnogo komismariata oborony SSSH. 1940. 59 P.
(Microfilm] (MLRA 7:11)
1. Russia (1923- U.S.S.R.) Armiya. Upravleniye voyeano-vosduoh-
nykh all.
(Airplanes--Recognition)

**I MO 0 0 Mg: 01" 0 0 10 & a a
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problem of jbv physicochernistry of surface phenmriess tn
-141 0- A
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of rl:)D.
of

AUTHOR: iatri?ey,,v, G. A.
TITLE: T h e Me can i c 3 o fo I ym c, r 7!,) 11
mol okul
PERIODICAL: Doklul,, Akade-ii iauk SSSR, I Vol 12.2. Nr
PP. 33'1-3~12 (USSR)
ABSTRACT: The authors first mention ani ~liscuso several previous pi,ors
It is -Jossible to consiler an expunded pclyrier chain as a
quas-i-elastic rod that contracts itself .0.on the externa,
fluence is diminislie~.,. This, pirienomenor, is -_ause,i by the
potential enerL;y which was a--raiiulated ~uri:-i_-- the
This process is reversible wl-.c~n there are ,.- _~ctivations cf t~ir.
valence bonds an,j .-ilen tll,t_-re are no co:iversicns The
observation of the elenentary act of tl;-, r-alture of the
elastically stresscd polymer is fundamentally important, f_~r
the mechanical pro~ertips of the polymer mrle,~ules The tl,er-
modynamic equilibrium of an elastically expana(--d Doleckilar
chain deponds on the ratio between the elastically stresscl
st4te of the inolecule and the influcace c.~f tl,.e external f.--ces.
For an estim-ation of this rati-~ and of th,-, inf,uence of V,e
Card 1/3 external forces or, the producti~,n of during- t!-.k,

The Wechanics of Pol~~,er 1-cle-c-,1--Z V/ z.-
mechanical rul)ture it Is 00fficir,nt to tai.i. i.-.tj
number of the val ence ton Is (n ) nf the ez: ~Lnde,i I o~nil
uner_y , whi cli i a ace umu I at ed du ri n,~ the e' %s ti ~ e7j'an3i on of
the molecular chwin, is vf,-ry int' 3t !!i 1hi. !~il'her
more si.-.iilar the expansion ener-y of the. !,i-.-it VaIt?,we 1,on,i
the dissociaticn ~ner-~y of th,? C-C-bond. V:ce arc reasl~,,13
suppose that the diss'i)ative processes tl:e
rupture of a af-E~ thC Fc, r
investi--ation of this probleifi it is not suffic:.,:,t t,~ cor-'fir-i:
oneself to the mcchanic iroperties of the
but it is necessary to take Lrtc accourit al3c, tl.e
the deformation of -,olymeric systems. A' i~.-csent t!ie
experimental inveoti,-ation of ti:e element%rj a-t of the elast,.:
expansion and of M-e merhani~-ai rupture of tl~e j-,lymer
is lm-~ossible I.-, the investif-ation of the r,ecanical defor7rai-
tions of the polymer body it has to be t~!ken into a-count ti-
possibility of elastic expansions ani of' theaecan-.cal rupture,.
of polymer molecules. These phenomena may be accompanied t;y
the production of radicals and by an activatio'. cf th~ valen-
bonds and, moreover, by dissipative processes An im-.c~rtant
Card 2/3 part of tI.,e pro,~ram reco-imendeiby the author is tLe investiralion.

The Mechanics of Polymer Molecules
SOV/2o-11-o-2-32/63
of the necanical expansion of polymer systems. There are 13
references, lo of which are Soviet.
PRESENTED: January 2, 1958, by V. A. KarEin, Member, Academy of SciencCE~
USSR
SUBMITTED: December 26, 1957
1. Polymera-Mblecaar stfwatw* 2. Nolevalar associatics
-Analysis
Card 3/3

PATRIUYEV, G.A.
Mechanics of the stretched polymer systems. Dckl. AN SSSR 120
no. 3:562-565 my 158. (MIRA 11:?)
1. Predstavlano skedemikom V.A. Xerginym,
(Polymers)

5(4), 15(9)
AjTHOR: Patrikeyev, G. A.
Parameters of
TITLE: The Correlation Betwecn theF2echanical Propertics and t:-.e
Structure of Stretched Pubber
P~,RIODICAL: Zhurnal f izicheskoy khii:,i i, 1 ~,-59 , Vol 5 3, Nr 9,
pp 2o8l - 2o89
ABSTRACT: This article presents data contained in a report held at t-.e
IX Conference on General Problems of the Chemistry anc, Phy-s-4-cs
of Compounds of High Mol,~cular 71cight. Supposing tl~,3t ar,
elastic elon-stirin (E) is determined by several polymer
cules forming an clasi~c network, a "mechanical" ti-,e-ry Cf
the molecular structare may be employed for thL invelti'lat
of stretched pcly.,:.cr systemo if the equilibrium, conciti-!.F
of the elastic ele::1c.,rts of this network are investi,atc-d
Accordin-ly, thcri! iijujt be a correlation (C) b(Avi,,un "'ne ;,a-
r,act(--ristico of th(; propcrtius of
(it) and tht-- externnI ctreoo f (equation (1)), rii, ii,(A, fiz; I,---
tween the mechanical and the str"ctural characteristics
tions (1) - (3)) (Ref 2). For the examiration of Jr. cja-
Card 1/3 tions (1) - (3), which detf--rL.,ine the equilibrium co.-Aitions

Parameters of
rilhe Correlation Between t~,e/h_'Ichanical ProLertics and thc
Structure of Stretched RubDer
between the mechanical and structural characteristics, a numLer
of (G)-sannples were investigated here with the use of Shopj)er's
0
tensile testinc machine. The value E (elasticity modulus cit-
0 CL
side the equilibrium in the test elcngation) varies but
with the dearee of vulcanization of natural rubber, but in-
creases by 2.5 times when the vulcanization of (R) is -,ro-
longed or the basis of sodium butadiene rubber (SBR), divinly!
styrene rubber (DSR), divinyl nitrile rubber (DNB), ~,nd poly-
chlorprene rubber, i.e. in the case of (R) on the basis of s~-n-
thetic rubber kinds of the structural type. The author irv-,'i-
gated the dependence of various characteristics or f; the re-
sults are given in a graph (Figs 4-12). The (C) which is de-
fined by equations (1) - (3) penmits an investi-at-ion of thi_.
stic elon6ation of polymer molecules in addition to elonga-
tions of the (R). It is recomnended to develop a new scientific
subject, the mechanics of stretched poly-mer systems (Ref 2) ~n
the basis of the reaultc obtained by the me(;hanics of poly-
mer molecules (Ilef 1). However, the instruments uat-d for
nical tests of (R)(by elonSation) arc, to be coLsicurably im-
Card 2/3 proved to obtain precise i:.easarements for the cvaluation of

Parameters of
~echanfcal Properties and
The Correlation Between the ri /1 -7
the Structure of Stretched Rubber
the mechanical and stractural characteristics. The aut!~zr tl-.an
Ye. A. Abramova and T. S. Dvorkina for their assistance ir, t:.,
present investiCation. There are 12 figures and 5 Soviet re.,er-
ences.
~f
SJDMUTTED: L.13rch 18, 1938
Card 3/3

S/190/60/002/009/019/019
B004/BO60
AUTHORS- Patrikeyev, G, A,, Gusarov, B. G., Konoplev, V. 1.
TITLE: Brittle Rupture oAj2jjmer8jin High-elastic State
PERIODICAL: Vysokomolekulyarnyye soyedineniya, 1960, Vol. 2, No. 9,
pp. 1436-1439
TEXT: Polymeric material weakened by incisions is bound to undergo a
brittle rupture at the incised spot at low temperatures and a certain
critical elongation rate. The autiltors checked this assumption by a
dynamometer and an M n0-2 (MP0-j)tj,1oop oscilloscope which allowed for
elongation rates to be measurea up to 2 m-sec-1. In natural rubber, the
tearing strength was found to be considerably reduce at an elongation
rate of over 0.7 m-sec-1 and temperatures of 20 + 59C. At.this rate,
a brittle rupture occurred at -60 0C, Figs, 1 and '~ show the experimental
data, The authors recommend the application of tearing strength tests
at high elongation rates. The need is felt of an improvement in inertialess
dynamometers. There are 2 figures and 2 Soviet references.
SUBMITTED: June 11, ig6o
Card 1/1

V(
13- '?.2-0c)
AUTHOR: Patrikeyev, G. A.
81868
S/020/60/133/02/44/066
B004/BO64
TITLE, The Molecular Mechanism Underlying the Deformations of
Polymeric Substances
PERIODICAL: Doklady Akademii nauk SSSR, 1960, Vol. 133, No. 2p
PP- 405 -- 408
TEXT: In the introduction the author states that the concepts hitherto
developed on the stressed state of an ideally elastic network and the
relaxation processes in the deformation of polymers have been derived
without considering a molecular mechanism. He discusses the possibility
of establishing the molecular m6chanism by way of interpreting the re-
sults of mechanical tests of rubber under the application of the meth-
ods of macromolecular mechanics (Refs. 11-13). From analyzing the
change of the cross section and the surface of an elastic body in the
case of extension, the author arrives at the conclusion that the geo-
metrical considerations alone indicate that a one-dimensional extension
is accompanied by complex three-dimensional translations of the
Card 1/3