SCIENTIFIC ABSTRACT DRAK, JULIUSZ - DRAKIN, SERGEY INVANOVICH
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CIA-RDP86-00513R000411120013-8
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RIF
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S
Document Page Count:
100
Document Creation Date:
January 3, 2017
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July 31, 2000
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13
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Publication Date:
December 31, 1967
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SCIENTIFIC ABSTRACT
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DRAN -TJO L Ia-
JXZIMO, Zdzislaw, dr. mod.. Wroclaw, ul. C.Sklodowskiej 40/8
Julius$
IMMA"'AWN
Secoudary mobilization of jeju-m in reconstructive surgery of
the esophagus. Polski przegl. chir. 26 no-9:769-776 Sept 54.
1. 111. Ilinika Chirurgiczna Akademil Medycinej we Wroclawiu;
kierownik dr. mod. Zo Jesioro
(ESOPHAGUS, surgery
plastic, with secondary mobilization of jejunum)
(JEJUNUM, surgery
mobilization in plastic surg. of esophWe)
r) t-C, I IL ); ~- 5 -4-
REOZEK, Halina; z
"12 ~ljul~luaz
Conservative treatment of i3echanical perforation, of the Intrathoraclo
esophagm.*Otolar. polska 11 no.4:391-396 1957.
1. Z Klin. Ieryngologicznej A.M. we Wroclawiu. Kierownik: prof. W.
Jankowski 1 2 111 Mus ChirurgiC2nej A. M. we Wroclawiu. Kisrownik:
doe. Z. Jezioro.
(ISOPHAGUS, perf,
management (Pol))
EXG~RPTA HEDICA See 9 Vol 13/2 Surgery Feb 59
1127. CICATHICIAL STRICTURC OF THE OESOPIIAGUS AFTER SURGICAL
TREATMENT OF PEPTIC VLCER DISEASE - 13liznowate zwczenie prze)yku
,po chirurgicznym leczeniu choroby wrzodowej - Drak J., J ezioro Z.
and K u d If. III Klin. Chir. Akad. Med., XV-PUEM'G. LEK. 1957,
12/49 (1892- 1896) Illus. 5 Wrociaw
Two cased are described. A difficulty in swallowing appeared on the 12th day
following the operation - In the first case resection of the stomach and in the 2nd
case gastroenterostomy. In both patients a very good remote result was obtained
by oesophagogastric anastomosis. The clinical course, the radiological pict4re
and the anatomical lesions found during the operntion In both cases showed that
the complication was a consequence of the healing of peptic oesophagitin. Oeso-
phaRogastric anastomosis in combination with resection In considered to be worthy
of recommendation.
_A
BCRON, Zdziolaw;QDRAK, Jultuell NUS, Henryk
Pnrtial and totnl diavhraguatic relaxation with aDecial referenCO
to differentinl diagnosis. Polski tygod.lek. 15 no.41:1566-1570
lo o 16o.
1. Z III Kliniki Chirurglosuej A.M.; kierownik: doc.c1r med.
Z.Jestoro i z Kliniki Radiologicznej A.M. we Wroclaviu; kierownik:
e
doo.dr mod. Z.Kubraki vi
(DIAPHRAGM d15.)
Kalignaut tumors of the small intestine. Polski tygod..Iak. 16 noas
.15-21 2 JA 161.
I. Z III Iliniki Chirmrgicsnej A.M. we Wroclaviu; Iderownik: doc.dr
med. Z.Jazioro.
(IMSTINE SKALL neopl)
(SARCOMA case reports)
MILEWICZ, Zygmunt;_RFA&,-Jullumz-_
A bonip gangllo-collular nouroma of-the mediastinum In the x-ray
picture. Polski pmagl. radiol. 25 no.61555-556 161.
1. Z.Kliniki Radiologicanej AM we Wroclawlu Kierownik: doc. dr med.
Z. Kubrakiewicz i z III Kliniki Chirurgicznej AM we Wroclawiu Kierownik:
prof. dr med. Z. -Tezioro.
(GANGLIONEUROMA radiog) (FXDIASTINUM neopl)
DILU"k, JulluBz
m
Me behavior rjf the contract melium "projjyl.l(;dorI-,.,'lagff in
tiBsue spaces after.exi.-arimentul perforation of the. esophagus.
Pol. przogl. radiol. 28 no.6:517-524 N-D 164.
1. Z III Klinlki Chlrurglcznej Akademii Medycznej we Wro-.lawiu
(KierownAt prof. dr. med. Z. Jezloro).
JEZIORO, Zdzislaw; DRAK, Juliusz; DRAKO'WA, Danuta
Apropos of the treatment of aardiospasm In children. Pol. tyg.
lek. 19 no.21:799-800 18 Myt64
1. Z III Kliniki Chirurgicznej Akademli Medycznej we Vxncla;jiu *
(kierownikt P--fe dre med. Ze Jezioro) I z I Kliniki Chorob
Dzieciecych Akadev~i Medycznej we Wroclawiu (kierownik: prof* dr.
med. T. Nowakowski,
TRAKY Juliusz; DRAKOWA, Danuta; GOLEN-TETER, Paris,
A case of perforated intestinal cyst in a child. Ped 4~at. Pol.
39 no.7&845-847 Je 164.
1. Z III Kliniki Chirur icznej AM we Wroclawiu (Kierowniks
prof. dr med. Z.Jezloro~ i z I Kliniki Pediatrycznej Akademli
Medycznej we Wroclawiu (Kierownikt prof. dr med. T.
Nowakowski).
DRAK, Julf.uv, GRIMSKI, Tadeusz; PIFGZA, Stanislwi; SO! -,Y:':, Wif-slaw
Benign t-.LTors of tne small Intestine. Pol. przegl. chir. 31'~
no.7;895-899 Je 164.
1, Z III Kliniki Chirurgicznej Akademii Modycznej we WrQi1aw1u
'X.erowniki prof, dr Z. Jezzioro) I z TV Szpl~tal Okrk~cwgo- e
a ~F '~
~roclaw-'u (Ordynatcr-, dr T. Orlow'sk!).
DRAK, Juliusot ORLOWSKIO Tadeuen
Intestinal invagiiiation in adultso Polo tyg. lek. 20 no.41142-143
25 X& 165.
1. Z III Kliniki Chirurgioznej Akademli 14edyoznel we Vroolawiu
(Kiorowiks profs dr. to Josicro) i t Oddzialu Chirurgicznego
Sapitals, Ckregovego we Woolaviu (Ordynatori dr, mod. T.Orlowski)f
BM"'311AT, MlenzyjItiv; BIIUWSrl, Tanj..-jz; J)~tl, Julbiri;,;
Malignan' -egencration of (,. J sinn anti of -a-ious
etlology. Pol. tyg. lek, 20n,).6t2Z4-Mj 8F
1. "' TIT Kliniki Chtrurgient-vj AkadiDm.u, I.L.".-%),,,!-awlu
(mur-6milce. prof. dr. 7. ~'Axlarzj). --
DRAK, Juliusz; HIRNLEO Zbigniewj MISTERKA, Stefan
Unusual etiology of an inflammatory tumor of the 110jum
simulating a malignant neoplasm. Polo przegl. radiol.
29 no-3:297-300 M~r-Je 165.
1, Z III Kliniki Chirurgicznej A14 we Wroclawi-i (Merown1k:
prof. dr. med. Z. Jezioro) i z Kliniki Radlologicznej AM
we Wroclawiu (Kierownik: doe. dr. Z. Kubrakievicz).
DRAK, Juliusz; BUGAJSKI, Adam; ZDOER, Zenon; SOLTYS, Wieslaw
Foreign bodies of the posterior mediastinum. Otolaryng. Pol.
19 no.3:397-399 165.
1. Z III Kliniki Chirurgicznej AM we Wroclawiu (Kierownik:
prof, dr. mod. Z. Jazioro).
MAUTAISKI) B. inzh,, nauch, trudnik
- -- - 'p- B~
Felletization of iron concentrates. Min d6lo 17 no.7:33-37n 162.
1. NIIH.
4.
NIKOLOV, A., insh.; DRAKALIISKII B., insh.; CIM=OV.. Iva.* in2he
Distribution of the eharde in the blast furnace top at the
Lenin Metallurgio PleAt. Min delo 17 no.9:20-26 S 162.
1,, Romitet po promighlenoptta, (for Nikolov)*
2, Nauohnoizaledovatelski institut po motalurglia (for
Drakaliiski and Charkezov)e
S
% -
DPJYJ,LIISKII, B.,,.-.inzh.-,- ..
Separation of lead by chlorinating pelletixation of
Kremikovtsi concentrates. Min delo 18 no.10t 23-30 0163.
1. VauchnoizoledovatelsId institut po chernata metalux-
giia.
ANISIWW9 G.M.; GALYAMICMp V.A.; GOLIDBERG, A.M.; DRAKE, A.D - -
.. ej
KTJZIMIN, Yu.M.; LYSOCHENKO, A.A.; MAGIROVSKIY, II.P.; FEDCSE'MPO.V.
Studying the operational conditions of the TDT-55 timber-skiddini
tractor, Trakt, i sellkhozmsh. no.11tl-4 N 165,
(MIRA 18:12)
1. Kafedra tyagovykh,mushin LesotekYnicheskoy akademii imeni Kirova
(for Anialmov., Ga.1yamichev, Gollberg, Drake). 2. Onezhskiy trak-
tornyy zavod (for Kuzlmin, Lysochonko, Magirovski7, Fedoseyev).
DRAKEI K.V.
I- -- -------
Action of Japanese elecampane on kidney function. Trudy Khab.med.
inst. no.20s193-200 160. (KIRA 15:10)
1. Iz kafedry farmakologii (zav, dotsent K,V.Drake)
Khabarovskogo meditsinskogo inatituta.
(KIDNEYS) (ELECAWANE)
DRAKE , K.V.
Diuretic action of birch buds. Trudy Khab.med.inst. no.20:212-
218 160. (MIRA 15:10)
.1. Iz kafedry farmakologil (zav. dotsent K.V.Drake) Khabarovskogo
meditsinakogo inatituta,
(BIRCH) (DIURETICS AND DIURESIS)
BFATETS,, Ye.T.; BEMNO., LoD.; GWASIMOV, A.I.; GOROVMO, L.I.j DMMG,
A. I. I DRUS L. V
Treatment of pulmonary-tubermaosis with phthivaside inhalationso
Vrach.delo no.11%341-11+2 N 162o, (KMA 3.612)
1, Oblastnot ptotivotuberkhleznyy dispanser g. Nikolayeva,
pervaya bollnitua g* Pikola-yeva, taberkuleznoye otdelenlys i
-detskly tuberkulsonyy sanatori-ya No.1 g. Nikola-yeva.
(TUBMMUSIS) (FMIVAZIDE)
VALUYSKIY, llikolay Tikbonoviebi POPOV, Ivan MikhWlovicb, kando ekonomo
red.; MARAKASOVA9
nauk; MOISEYEV, M.I., red.j P~~~Ajjq
L.P., tekhn. red.
[Undivided funds are the foundation of commnal econor7l Wedelinye
fondy - osnova obshchestvennogo khoziaistva kolkhozov. Pod obshchei
red. Moineeva M.I. Moskva, Izd-vo "Sovetskaia Rosaiia, " '1961 23 pe
(MIRA i4:11)
1. Predsedatell kolkllbza "Pobedall Kantemirovskogo rayons. Voronezhskoy
oblasti (for ValuyskJy % 2. Chlen-korrespondent Vsesoyuzncy akademii
sellskokhozyaystvenwjkh nauk im. V.I.Lenina (for Yloiseyev).
~ (Collective fams-Finance)
t 44729-66 EWTW/FW(e)/ZR(t)ZMT upcq) _.tnA,,vAz
ACC NRs AP60 4 SOUCE CODE,..- W0Q-w6q
AUITIOR: Pavlovskiy., M.:N.1 _P, 73
OFG: none
TITLE; Concerning the metallic phase of ca*on
SOURCE: Zhurnal eksperimentallnoy i teoreticheskoy fiziki. Pialma v redaktalyu.
Prilozheniye, v. 4., no. 5,, 1966j 169-172 ,
TOPIC TAGS: carbon, metal propertyp phase transition, high pressure researchp
graphite, shock wave propagation
ABSTRACT: The authors investigated the shock compressibility of graphite in the re-
gion of its bypothetic transition into the metallic phase.. The method and the mea-
suring apparatus are described in earlier papers (with L. V. All huler et al, Fiz.
iAl'
aV~ te 1
tverdogo tela v. 5, 279, :L963 and earlier). Synthetic hite 1.77 and 1.85 9,/cmF)
3
and Ceylon graphite pressed from finely crushed powder 2.23 c 3) were used. The
cM
2 23"
resultant plot of the pressure against.the specific volume (P-V) is compared with the
data of N. L. Coleburn (J. Chem. Pbys. Y. 40, 73P 1964) and with the results of B. J.
Alder's and R. H. Christian's dynamic measurements of the compressibility of graphite
(Phys. Rev. Lett. v. 7, 367, 1961). Satisfactory agreement between the authors' data
qLnd the results of Alder and Christian is observed up to pressures of the order of
600 kbar, but a great disparity is noted in the pressure region 600-900 kbar, where
Alder and Christian conclude that the graphite becomes metallic., whereas the authors
Card
L W4729
ACC NRg
0
find that the shock adiabat in this pressure region is merely a continuation of the
adiabat of the tetrahedral modification of carbon. To explain the causes of the dij-
parity and to obtain absolutely unique results with large measurement bases, the
authors developed a large-scale measuring apparatus with an explosive charge of 600'
mm diameterp imparting a velocity -5.6 Rm/sec to a steel striker 5 mm thick, and
tested two-layer samples of synthetic and Ceylon graphite., 7be wave velocities were
measured in each layer separately. The values obtained f6r the shock compressibility
of the graphite at pressures 1.55 Mar and 3-25 Mar demonstrate that the Alder and
Christian claims of observation of a metallicphase of carbon at pressures -8W kbar
are in error. They were apparently obtained with samples whose thicknesses did not
correspond to the striker thickness) and consequently, the parameters of the shock
wave In the graphite were distorted by the relaxation waves* Orig. art. has., I
figure.
SUB CODE: 20/ SUBM DATE: 1_1Jun66/ ORIG REF; 004/ OM RV: 006
Card
DRAKHLI, M.Ta., podpolkoynik moditainakoy aluzhb7.
Epidemiological abservations In epidemic parotitis. Toon.-mad. shurs
no.9:61-63 5 151. OUL 9:9)
(HUMM)
DRAMUN, M.Ya. (Perml)
.,eroes in thi) oolution to hic-aU ,~
Mat. D0-508-64 165- (KIFul, 38:20)
DRAKHI,lN, M.Ye. (Perm')
---Some prlnc~pies or comparison for Riccati differential equations.
Izv. vys. ucheb. zav.; mat. no.3174-77 165. (MIRA 180)
DRAML111, YE.
USSR/Phries - Rest Exebange MAY 52
"Thermal Convection in a Spherical Cavity," Ye.
Drakhlin, Molotov State U
"Zhur Tekh Fiz" Vol )=It NO 51 PP 829-831
Solves the problems of weak.. freep stationary con-
vection in a spherical ervity at a specified temp
gradient toward infinity by the method of power-
cxpansion of Grasshof's number and by using the Ist
approximation for the temp and the 2d approximation
for the velocity. Received 31 Jan 52.-
2=85
DRAXT=_ Ye, - Rh -
=7Ph3FEfic6'--'Convection FD-657
Card 1/1 : Pub. 85 - 12/20
Author : Drakhlin) Ye. Kh. (Molotov)
Title : Convection in an infinite horizontal elliptical cylinder
Periodical : Prikl. mat. i mckh.p 18) 215-218, Mar/Apr 1954
Abstract : Sets up the equations and boundary conditions for convection in an
infinite horizontal elliptical cylinder. Obtains the zero approx-
imation and the first approximation. Three references including the
author's earlier work in Uchenyye zapiski Molotovoogo Universiteta
(Scientific Notes of Molotov University) Volume VIII) 1953.
Institution
Submitted January 20, 1953
Abet Journal: Refamt Zh= - Mekbanika,, No 3, 1957, 3183
Authors Drakhlin, Ye. Ma.
lastitutions None
Titlet Free Stationary Thermal Convection in a Spherical Cavity in the Absence
of a Threshold,
Original
Periodical: Uch. zap. Molotovsk. un-t, 1955# 9j, No 4, 29-39
Abstractt An approximate solution is obtained for the problem of the stationary
convection in a liquid or gas medium filling a spherical cavity in the
mass, when a constant temperature gradient, having any direction but
not vertical,. is specified in the mass at infinite.
The problem is assumed to be plane.
The equations are solved by a successive-approximation method, based
on expanding the solutions in powers of the Graashof number.
Card 1/2
Abst Journal: Referat Zhur Mekhanika, No 3, 1957, 3182
Autb,or: Drakhlin,, Te. Kh.
Institutionl None
Title: Free Stationary Thermal Convection in a Space Bounded by Two Coaxial
Horizantal Lifinite Cylinders
Original
Pericdical: Uch. zap. Molotovsk. un-t.: 1955, 9. No k, 41-47
Abstract: An apprcocimate sol*.ion Is given for the problem of the stationary
cc,nvection In a liquid or gas medium filling a cylindrical alit,
bo'unded by coaxial circular infinite horizontal cylinders, when a
c"stant temperature gradient, perpendicular to the axis o T~ e
cylinders but not vertical, is oftecified in the mass at in inite.
It is assumed from s~*etry contraeration that the problem Is a k.
plane oDe.
Card 1/2
Abst Journals Referat Zhur - Mekhanika) No 3, 1957, 3182
Abstracts The equations of the thermal stationary convectic'n are solved by a
successive-4pproximation method, based on expanding the solution in
powers of the Grashof number. The temperature distribution in the
liquid and in the external and internal masses are found in the zero
and in the first approximations and the distribution of the hydro-
dynamic velocity of the liquid is found in the first approximation.
Card 2/2
U3SR/At=ic and Molecular Physics Heat, D-4
Ab!jt J.--urnal: Referat Zhur - Fizika, No 12.. 1956) 3441l
Auther: Drakhlin) Ye. Kh.
------------ -
Instituticn: None
Title: Free Stationary Thermal Convection in Spherical Cavity in the Absence
of a Threshold
Original Periodical: Uch. zapiski Molotovsk. un-t., 1955, 11, No 4, 29-39
Abst-ract: Investigation of the steady-state free thermal convection in a liquid
fillirg the spherical cavity, surrounded by a solid mass for which there is speci-
fied, far from the cavity, a temperature gradient that is constant in space and time
ard has any nonvertical direction. The hydrodynamic equations are used in the usual
approximation of convection theory. The boundary conditions are chosen to agree
with continuity of the temperature and of the thermal flux and with the presence of
an adhesion layer. The solution is sought under the assumption that the flowlines
are in the parallel planes, determined by the direction of the tempereture gradient
ir the solid body far from the cavity, and by the vertical direction. To obtain the
solution, successive-approximation method is used, in which the functions that must
1 of 2 - 1 -
USSR/Atcmic.and Molecular Physics - Heat, D-4
Abet Journal: Referat Zhur - Fizika, No 12, 1956, 34411
Author: Drakhlin, Ye. Xh.
Institution: None
Title: Free Stationary Thermal Convection in Spherical Cavity in the Absence of a
Threshold
Original Periodical: Uch. zapiski Molotovak. un-t-, 1955, 11, No 4, 29-39
Abstract: be determined are sought as power series of the Grasshof numbers. The
corresponding equations are solved rigorously in each approximation. The zero and
first approximations obtained for the zeibperature and the zero, first, and second
approximations are obtained for the velocity. In the first approximation the current
lines turned out to be circles, and the central part of the liquid rotates as a whole.
2 of 2 2 -
~) (k rN K ~A I I' V1 :41 ~e. . ~- L'
USSR/Atomic and Molecular Physics - Heat, D-4
Abst Journal: Referat Zhur - Fizika, Fo 12, 1956, 34412
Author: Drakhlin, Ye. Kh.
Institution: None
Title: Free Stationary Heat Convection in a Cavity, Bounded by 2 Coaxial Horizontal
Infinite Cylinders
Original Periodical: Uch. zapiski Molotovsk. un-t., 1955, 11, No 4, 41-47
Abstract: Discussion of the stationary free thermal convection in a liquid that
fills a cavity bounded by 2 very long coaxial circular cylinders, separating the
liquid from a solid body. A temperature gradient that is constant in the space and
in time and directed perpendicular to the axis of the cylinders (but not vertically)
is specified far away in the solid body. The problem is a plane one. It is assumed
that the temperature and heat flow are continuous on the boundary between the liquid
and the solid body and that an adhesion layer exists. The usual convection equations
are solved approximately using expansion in powers of the Grasshof number with the
corresponding equations being solved rigorously in each approximation. The zero and
first approximations are obtained for the temperature of the liquid and of the solid
and for the velocity of the liquid.
/ a-c/ - 1 -
DRAkIkIll-Ity, K,K//Y.
ATJTHORs DRAKHLIN, Ye. Kh.* rml 40-5-11/20
-spa
TITLEs The Solution of the Equation for the Case of Stationary Heat
Convection in an Infinite Inclined Circular Cylinder (Resheniye
uravneniy dlya odnogo sluohaya statsionarnoy teplovoy konvektsi".
v beskonechnom naklonnom krugovom tailindre)
PERIODICAL: Prikladnaya Mat. i Mekh.,1957,Vol-21,Nr 5,pp.693-695 (USSR)
ABSTRACT: The author found rigorous solutions for the problem of sta-
tionary heat convection in the medium part of an extended,
inclined circular cylinder. The cylinder is assumed to be in a
fixed body with a temperature gradient constant in the space as
well as with the time. It is supposed that the streamlines are
parallel to the axis of the cylinder, and that there exists no
temperature gradient along the cylinder axis. Applying the gi-
ven suppositions it is possible to transform the initial equa-
tions for the heat convection of the cylinder in such a way
that rigorous partial solutions can be found. The solutions
can be transferred to the limit cases of the vertically stand-
ing and of the horizontally lying cylinder and then give aolu-
tions which have been already investigated by other authors.
For horizontally lying cylinders with vertical temperature gra-
Card 1/2 dient only a solution with vanishing velocity of flow is pos-
The Solution of the Equation for the Case of Stationary Heat 40-5-11/20
,Convection in an Infinite Inclined Circular Cylinder
sible.-This cannot be expected in another way according to the
assumption of axial-aymmetrio velocities.
There are no figurest no tables, and 2 Slavic references.
SUBMITTEDs April 24P 1956
AVAILABLE: Library of Congress
Card 2/2
DUKHLIN, Ye.n.
Stat lonory-conveat ion equat ions. ITauch,,dokl,vys,sb'col7; fiz.-mat.ra-*,-I
no-5:71-77 158. (MIRA 12:7)
1. Pern-skiy gornyy institut.
Oleat-Convection) (Functional equations)
32495
0 0 3/044/61/000/011/017/049
C111/C444
AUTHOR: Drakhlin, Ye, Kh~
TITLE: '~i~heapp ~icai`ion o~fthe method of successive approximations
on the equations of heat-convection in the case of the
three-dimensional problem
PERIODICALi Referativnyy zhurnal, Matematika, no, 11, 19061, 41,
abstract llB207,.(Sb. nauchn. tr,. Permsk gorn in-t, 1959;
no. 4, 79 - 98)
TEXT: By aid of the Green functions of the harmonic and the bi-
harmonic operators the author reduces the system of '~he three-dimen-
sional heat-convection, consisting of five equations, to a system of
64 integral equationsl lie proposes to solve these by successive appro-
ximations. Further on the author falsely claims that the second and
fourth derivatives of the Green functions of the harmonic and bihar-
monic operators are absolutely integrable, On this base he derives
conditions for the convergence of the successive ap:,roximations.
[Abstracter's note: Complete translation.!
Card 1/1
32524
16, 5 SV0 141 5,30 o S/044/6!/000/011/047/049
CIII/C444
AUTHOR: Drakhlin, Ye. Kh.
_4_~
TITLE: The application of the secant method to the equations of
heat convection in the three-dimensional case
PERIODICAL: Roferativnyy zhurnal, Matsmatika, no. 11, 1961, 43,
abstract 11V248. (Sb. nauchn. tr. Permsk. gorn. in-t..
1959, no. 4, 99-113)
TEXTs The system of equations describing the free stationary
heat convecti3n in a certain domain 0) with the closed boundary S 0, is
solved by aid of the secant method. One introduces a vector Cx, Y, Z)v
the components of which together with all its derivatives up to the
fourth order inclusively belong to the space of the continuous functiors
C(co), and a function e(x,y,z) which together with its three partial
derivatives of first order belongs to C(W). On the initial equation
the operation "red" is applied and one passes over to a system of four
equations in dimensionless variables. Under the supposition that the
first boundary value problem for the Laplace equation and for the
biharmonical equation possesses its Green functions in CO, the obtained
system is reduced to a system of seven integro-differential equations.
Card 1/2
32524
S/044/61/ooo/oll/047/049
The application of the secant . . . C111/C444
To the latter a modified secant method is applied, the successive
approximations being determined according to th o formula V1(
Xn+1 , Xn - 0 (xn) (a-xo).
It is proved that in the modified secant method the successive
approximations converge to the solution of the initial equation, an-j
that this solution is unique under certain ccnditions.
[Abstracter's notes Complete translation.]
Card 212
~v AO! 11"I":~', ir4v~~4ff XWC rw
922cma --------
~~es cri the s ta%i,na.7;-
c,,%-inder
4.1
(Sb. na-i-,chn. tr. Perm-sk. t~ollitel&n. in-t, no. 7, iss.l, 19L-A) 67-75
-,c-m o' e-quatiorz 'or st-tiorary heat convect4 `n s lopec
-!-3 tern c f
A. S/044/61/000/011/018./049
C111/C444
AUTHORs Drakhlin, Ye. Kh.
TITLE: On the convergence of the process of successive approxi-
mations for the equations, describing the stationary
heat convection in an infinitely inclined cylinder
PERIODICAL: Referativnyy zhurnal, Matematika, no. 1t, 1961, 41,
abstract 11B208.(Sb. nauchn. tr. Permsk. gorn. in-t,
1959, no. 5, 124 - 136)
TEXT: Described is the same method as in the above referred
article (Ref. 11BI07)- Yet the assumption of the flow being plane in
the tube simplifies the equations and permits the author to avoid the
formerly made mistake.
Abstracter's notex Complete translation.]
Card 1/1
L 19411-63 EPR/EVI(1)/EPP-(c)/Epp(n).~2/BDS AMCIASI)ISSD .'r_'3-4/Pr-4/Pu-4
ACCESSION Mi: AR300078 S/0044/0/000/06WBOWBO65
SOURCE: RZh. Matem~tikaj. Abe.-_6B288-
ATMOR: Draltain, Y6. Kh.
MLE: On equations of the three-dime:tional problem of convection theo
CITED SOURCE; Sb. nauchn. tr."Pormske politekhn. in-t, no* 9) 1961S 103418
:TOPIC TAGS! differential equation
convection theory
IZA~NSIATION: The author considers the boundary problem for equations describing-
free stationary thexmU- c6nvection'within a sphere S if on the surface o~C the_-
sphere -the velocity is equal to zero and the temperature is spgc=eds----___
d1v v-0.
-0. 'T"IS-4p (S),
The solubility of this problem is proved for the case of small resultant velocities
and temDeraturess It is shown that Newton's method is applicable to the solution,
of the problem. K. Oolovkin.
DATE kQQt 24Jul63 SUB COM MH ENCLi 00
Card-1/1
ACCFSSIOII NR: AR401h415 8/0124/64/000/001/~02/W62
SOURCE: RZh. I*khanika,, Abs. 1B514
AUTHOR: Droldilin, Ye. Kh.
.JITLE: F4 uatJonc of the three-dimensional problem of the convection theory
CITED SUMM St. nauchn. tr. Pernisk.' politekhn. in-t, no. 9, 1961, 105-118
TOPIC TAGS: convection, heat convection, three-dimensional convection
TRANSIATION: The boundary problem for equatl6ns describing the free stationary
heat convection vithin a sphere 9 has been described for the case when the veloc-
ity is zero at the sphere's surface,'and the temperature is given by
d1vv_0
The solvability of,this problem for small resulting velocities and temperatures
Card 1/2
ACCESSION NR: AR4014415
has been shown and the solution can be found using Newton's method. K. 0olovkin
DATE ACQ-,. i8peb,64 MM CODE: Alp PH ENCL: 00
Cord 2/2
KOMGIN, L.P.. kandidat teklmicheskikh nauk, dotsentj j1JI" Te.Te.,
inshener; PATLOV, M.S., inshozer,
Investigation and improvement of existing water softeners used
by the railroads. Sbor.LIIZHT no.150.-120-148 156. (MU 9t1l)
(Yeed-water purification)
DRAXHLIN, Ye,Ye,, insh,
Using contact water purifier# at railroad stations. Sbor. LIIZHT
no.152:69-79 158* 041RA 1116)
(Food-water--Purification)
(Railroads--Water supply)
KORTAGIN, L,]Po, dotsent, kand.takhno nauk; DRAK,HLI#,,.,TgpTr,.,, jazh.
...
Removal and use of sediment rom calcium-soda water softeners*
Sbor. LIIZHT no.152:80-127 158. (MIRA 11-6)
(Food-water purification) (Railroads--Water supply)
DRAHLIN, Ye.Ye., inzh.
.
investigation of tho operaticn of a now kind of thermochemical water
softener. Sbor. trud. LIMIT no.185:130-,143 1620 (MIRA 17g1)
MAY IS, inzhoner-kapitan
Ground training of flight pereonnol Is a good idea.
Tent.Vozd.Fl. n0-7:83 J1 160. (HIM 13:7)
(Ylight training)
AID P - 3700
Subject USSR/Electricity
Card 1/1 Pub. 29 - 5/25
Author : Drakhman, D. L., Eng.
Title : Removing steam corrosion of boiler pipes
Periodical : Energetik, 12, 110 D 1955
Abstract : The author describes a case of corrosion of boiler pires
of a Clark Chapman boiler which worked for It" years without
defeat. In 1950 the steam separating equipment of the
boiler was remodeled and shortly afterwards trouble began.
Some pipes burst and heavy steam corrosion was found to
be the cause. The author describes preventive measures
applied. One drawing.
Institution : None
Submitted : No date
DRAKIN, Aleksey Ivanovich; SOKOLISKAYA, Zhozefina Markovna)
2bm-mltvt;--POMp A.S.., red.;'ZAYTSEVA, L.A., tekhn.
red.
[Organizer of mass production work) Organizator proizvod-
svenno-massovoi raboty v profgruppe. Moskva, Profizdats
1963. 43 p. (Bibliotechka profsoiuznogo Ektivista,
no.22(70)) (MIRA 17:3)
1. Predsedatell zavodekogo komiteta profsoyuza Elektro-
stallskogo zavoda tyazhelogo mashinostro7eniya, Pod-
moskov'ye (for Drakin).
SOV/58-59-4-8%9
Translation from: Referativnyy Zhurnal Fizika, 1959, Nr 4, p b1 (USSR)
1AUTHOR:
ITITLE:
Drakin, A.V.
Noise Diode for 10-cm Range
I PERIODICAL: Izv. Leningr. elektrotekhn. in-ta, 1958, Vol 36, PP 158 - 166
1 ABSTRACT:
The author describes the design of a noise diode intended for the measure-
ment of the noise factor of radio receivers in the 10-cm range. The diodej
is made in the form of a coaxial line loaded from both ends by wave guides.
To excite the wave guide the ends of the cathode protrude from the anode.
The design assures the strain of the tungsten filament of the cathode in
the hot state. The author provides expressions for calculating the power
of the noise. He describes the methods of measuring the noise factor of
the receiver. Cf also J. Inst. Electr. Er4pig, 1946, Vol 93, part IIIA,
1436.
Yu.B. Chernyak
Card 1/1
01.~ i.J.,Croas.
7rakin (".r, .
.!e Yl
VF, C, :"Ilr n r t. T 0 UC r, V j t
or,
d b.
r'r~,bl -rm uni
.3, Snrin;~ so.! pj-~~P-,ratinr.3, t1he
crtiii -
-31,.",
1n;, !ird thi tl,-inqpo.,-t-:ti on of t-..z b. AF, .
DRAKII',~~, G. G., Cand Agr Sci -- (diss) "Efficiency of square-hill chec?.
and square methods of' raising sugar beets under the conditi-cris of' Kuban . "
Krasnodar, 1060. 16 pp; (Ministry of Agriculture Xuban Agricul-
tural Inst); 150 copies; price riot given; (KL, 2/-6Cj, 1561,
SZVJYAMV, P.M., insh. L DRABUN, G.Ho, lush.; GAMNA, N.Z.. arkhitaktor;
TISHIN, A.M., a~k-hil-telrbr--
Standardization of auxiliary construotion elements of multistoried
industrial buildingp. Prom. stroi. 3B no-10:52-57 16o. (miRk 13:9)
(Factories-Design and construction)
(Stiireasso-Standards)
5/147/62 ~000/001/008/015
le, 57/0C E191/E135
AUTHOR: 2Ea~~.
TlTLE. Determination of the optimum geometry parameters in
the design of aircraft
PERIODICAL; Izvestiya vysshikh uchebnykh zavedeniy,
Aviatsionnaya tekhnika, no.1, 1962, 66-74
TEXT: The criterion of optimisation for the design
parameters of an aircraft is the achievement of the lowest take-
off weight for a given useful load and given flying qualities,
since it is assumed that the cost of the aircraft is proportional
to its take-off weight. For convenience in this analysis, a no-
called ballistic drag coefficient is introduced, defined as the
drag coefficient divided by the wing loading. A change in any
geometric parameter of the aircraft changes the take-off weight
in three ways. 1) The relative contribution to the total weight
of the aircraft portion directly measured by the particular
parameter. 2) The ballistic drag coefficient changes, causing a
change in the fuel carried. 3) The 'scale effect' causes a
Card 1/3
Determination.of the optimum goo S/147/62/000/001/008/015
E191/E.135
further change in the relative weight of the aircraft portion
and in the ballistic drag coefficient. The scale effect is the
effect of the overall size of the aircraft on the relative
weight and drag contributions. The condition of minimum overall
weight is introduced and the general case is formulated in
analytical terms leading to a formula by which the rate of
change of relative weight as a function of the geometric parameter
divided by the rate of change of the ballistic drag contribution
due to that parameter must be equal to a certain quantity which
can be described as characteristic for the aircraft in question
and whose computation is given. In the case of geometric
parameters which interact with each other, two simultaneous
equations are obtained which have to be solved together. By
way of example, the optimum wing loading is examined at a given
fly'ing speed and flight altitude. )1aking certain approximations,
an explicit formula is obtained. A second example of the
optimum slenderness ratio of the nose portion of the fuselage is
examined. The optimum value is shown to depend on the skin
friction coefficient and the mean I-Aach number.
Card 2/3
Determination of the optimum ... S/147/62/oOo/ool/oo8/oI5
E191/E135
The formula so obtained is applicable to the optimum slenderness
ratio of any cylindrical body in the front section, whose axis
is parallel to the general flow.
There are no figures or tables.
ASSOCIATIONs Kafedra 101, Moskovskiy aviatsion'nyy institut
(Department 101, Moscow Aviation Institute)
SUBMITTEDt November 16, 1961
Card 3/3
15
PH= I BOOKmawITATION SM15623.
Drakin, 1. 1.
Aerodinamicheskiy i luchistyy nagrev V polete (Aerodynamde and Radiative
Heating Daring 7light) Moscowp Oborougizp 1961, 94 p, Errata slip inserted.
5,8W copies printed.
Sponsoring Agencyt. Ministerstvo vysshego i arednego spetsiallnogo obrazovaniya
RSFSR.
Ed.: K. Ya. Zayteeva.. Engineerj Ed. of Publishing House, N. G. Kopylovaj
Tech. Ed.: V. P. Rozhin; Managing Ed*: A.S. Zaymovs"ya., Engineer,
PXMM: This textbook is intended for technical schools of higher education and
will be useful t9 aspirantsp teachers, and engineers specializing in the field
of gas dynamic and radiation beating.
COVERAGE: The book describes methods for determdning the temperature of the outer
skin in aerodynamic and radiation beating in flight. Stationary and non-
stationary conditions of thermal processes an discussed and working formulas
Card-t(5
Aerodynamic and Radiative Beating (Cont.) 507~~r,621
as vell as, tables of physical data are given6 Examples of con;ilic&ted, compating
methods am gVren, No personalities are mentioned. There an 53 references:
37 Sa-riet (including 8 translations),, and 16 English.
TAME OF C 8:
Foreword 3
Conventional Designations 5
Ch. I. Heat Exchange in Aerodynamic Beating 7
1. Heat flows at the surface of a body in flight 7
2. Heat transfer coefficient in the flow over a plam plate
at ze-ro angle of incidence 12
3. Heat transfer coefficient the flow over an inclined plate,*
~
tion
airfoil,and a body of rev 1T.
4* Heat transfer coefficient the f1w over leading surfaces 23
5. Factors influenciM the transition laidn to turbulent
bcPandary layer 25
66 Special features of beat transfer at hypersonic velocities 36
Car&-2713-
69317
1000 S/147/60/000/01/006/018
10~Uuo E191/E581
AUTHOR: Drakin, I.I.-
-----------------------
TITLE: The Effect of the Variations of the Weight and Aero-
d namic Characteristics,,~f a Designagon the Flying Weight
of a Flying Machine
PERIODICAL: Izvestiya vysshikh uchebnykh zavedeniy, Aviatxionnaya
tekhnika, 1960, Nr 1, PP 52-62 (USSR)
ABSTRACT: The derivations are applicable to an aircraft or guided
missileA The effect of the weight and drag of the
separate units and of the specific thrust (ratio of
thrust to the rate of fuel consumption) of the power unit
upon the total weight of the flying machine are evaluated
when the performance and useful load are kept constant.
To do so, requires the change in all the units of the
design when one unit is modified. Thus the wing area,
if altered, requires the modification of the power unit,
the fuel. reserve, the fuselage size and others. The
performance is determined by the total weight, the fuel
reserve, the thrust of the power unit, the specific
Card 1/4 thrust, the aerodynamic drag and the lift. The relation
69317
S/147/6o/ooo/01/006/018
E191/E581
The Effect of the Variations of the Weight and Aerodynamic
Characteristics of a Design on the Flying Weight of a Flying
Machine
specific thrust, each with the appropriate derivative.
The take-off weight is the sum of the useful load, the
structural weight and the fuel load. From this equation
the derivatives just mentioned are deduced. For the
derivative in respect of the structural weight, use is
made of weight formulae (e.g. Fomin. N.A. "On Methods of
Determination of the Basic Parameters of-the Aeroplane
and its Wing", Trudy MAI, Issue 108, Oborongiz, 1959
and Shanley, F.R., quoted in Russian translation:
"Weight and Strength Analysis of Aircraft Structures",
Oborongiz, 1957). For the effect of the drag on the
take-off weight, the present author's derivations on
the required relative fuel weight are used ("Determination
of the Required Fuel Reserve for a Flight at Variable
Speed and Altitude", Trudy HAI, Oborongiz, 1960). In
obtaining the relevant derivative, the variation of fuel
Card 3/4 weight is assumed to include the weight of fuel containi
69317
S/147/60/000/01/006/018
E191/E581
The Effect of the Variations of the Weight and Aerodynamic
Characteristics of a Design on the Flying Weight of a Flying
Machine
means. In deriving the effect of specific thrust, this
is assumed constant during the entire flight. Some
approximations made depend on the extent of take-off
weight variations examined. It is recommended that
take-off weight variations exceeding 50% should be
treated in several stages. A short discussion is
devoted to the constituent parts of the specific drag
namely the part dependent on the total weight, the part
corresponding to the power unit and fuel volume and the
part corresponding to the useful load volume.
There are 1 figure and 5 references, 4 of which are
Soviet and 1 English.
ASSOCIATION: Kafedra LA-1, Moskovskiy aviatsionnyy institut
(Chair LA-1, Moscow Aviation Institute)
SUBMITTED: January 15, 1959
Card 4/4
MAKIN, I.I.
Determining optimum geometrical parameters of airplane structures
Izv,vys.ucheb.s&v.j av.takh. 5 no.lt66-74 162. (?aR& 16M
1, Moskovakiy aviatsionnyy instituts, kafedra No.101.
(Aeroplanas-Detaign and caretruction)
DRAKIT, I.I
Method for economic analysis of the reliability of aviation
parts ajid systems* Izv,vys,ucheb,zava; av.takh. 5 no.31
177-186 '162. OaRk 150)
(kirplanea-Design and construction)
(V) IJP(C) W~ 'D
-6 W(d)/W(M)/WP(
-~L 0-6 ~23 _py7r~j (k)L 1)j
T6031848 So E CODE: UR/0000/66/000/0(
AUTHOR: Drakin, 1. 1. (Candidate of technical sciences)
ORG: none
TITLE: Design and selection of materials for the thermal insulation of aircraft
SOURCE: Metody raschetov temperaturnykh poley I teploizolyataii letatellnykh apparatov
(Methods for the calculation of temperatxne fields and heat insulation of aircraft);
sbornik statey. Moscow, Izd-vo Mashinostroyeniye, 1966, 35-76
TOPIC TAGS: thermal insulation, aerodynamic heating, insulating material, ablative
heat transfer, heat conduction equation, mathematical analysis, heat transfer, instru-
ment panel, radiant heating, thin airfoil, approximation method
i
STRACT: The use of various types of thermal Insulation for aircraft was analyzed.
e basic insulation parameters were derived by approximate calculation methods for
fferent conditions of kiuetic gas heating..- A comparison was made of different types
insulation, including ablative materials,*and their utility under various condi-
ons. Equations were given for the necessary insulation mass on 1 M2 of its surface.
en plotted as a function of time, it showed that the heat insulating properties of
at imsulating materials were satisfactory during rapid heating. One-dimenalonal heal
nduction equations are presented for coating type Insulation, and methods of solu-
qqrd . 1/2
on were outlined. The heat exchange equations were simplified by assuming the Biot
mber to be constant; the resulting solutions were given for both a constant and a
anging equilibrium temperature. An approximate determination of the necessary thick
ss of insulating linings was derived from a consideration of the temperature differ-
ce on the internal surface and the Fouri umb r An analysis of the criteria for
ideal insulator showed that P/017r2 :hold'be proportional to the mass of
(1314 1 N
of insulation. The use of insulating_coating;k different portions of the aircraft
a anag zed by means of appropriate heat transfer equations. The temperaturedistri-
,tionl- a metal sheet with a thin insulating coat and the necessary thickness of
is coat were approximately detemined. Among coating materials considered were
oxies, resins, and ceramics. For the Insulation of instrument compartments, the fol
wing topics wer* Included: the heat generated in a compartment, the heat capacity
instrumentation, the equivalent coefficient of air heat conductivity and radiation
at transfer in the ocapartment, heat transfer equations for the Insulated compart-
nt. the influence of flight altitude on the temperature of the chamber,'the influ-
C f air layer thichmse, and the degree of darkness, and the Internal heat shield-
V instrame t compartments with appropriate materials. Orig. art. has: 13 figures
;
table, 07 fanwlaa.
COVEI 01613/ SON DATE: 25NavG6/ ORIG PEFt 016/ OTH RM 005,
D 121A PI) t,) L , A],
DZWAMDZA, V.11.; IMA 1. L.A.
Studying the coking ofMorgian coal with semicoke. Trudy Inst. not.
i gor. dela AN.Gruz. 8n 2:233-248 149. (MIRA Iltl)
(Georgia--Coal) (Coke ovens)
r1
d%~ IMWt"
at
0 "llu
Cridte 2
1
a
Pat tol
.
GrWn.
dectrol
lM.OH
conspa.
be rM I
"d ealk
-MOZ.-
kd dw=pWdm of wage Hqw hm
woduttlen and Its utilization P N D fin.
A. MWn (Metal and MIX"S "w. Aft'd.
S.S.R.. Tiflis). Soobshzheniyu Ah4d. Nauk
Ito 647-UJI9301in Russfam).-Practical
t sulfite I quor s fewdble as a sounv a(
:pf"m the absorption of 6% tonned hem de-
anodic liquor (1). T'he resulting Na#90. can 1
to lon. Didn. of I yields org. adds
t an themat decon pn. yields 8%
L ppended. . -0. M. Kowlapoff
I rocks k Tk&W'sk coals. P.N.Whateridreand
Der. PrOls4, K4imm. 271 all-DOIRM).-
COR Is "4"n arc hetef ote. ConsIder..-
ablq quantities of fossil resins whMareeoutoou"r'd Its cAvItIcs of
different shapes anti in veins, The poisible origin of the--m
bodies 6 d6cusmd at great length. When hrmted vis to
32D-M' thtse resins begin ta melt with sorne demrspn. and
about 15% of a Autif liquid, brown and with a characteristic
Odor, Sep$. out. n Ch of on of the sever-d
t recorded Is SICZ ;%: 'FMIS, A'1A 31.05p CaO
L B-ncowitx-
Kcsksokhimicheskaya laboratoriya Instituta met&U& i gornogo dele A"de~!I-nauk
Gruzinsk6y-SSR.--
DIRAKIN, L. L.
DRI ", I "I L. A. .- "Investigation of p)~cnolz~ in Itlic t,~r (.f'
71dLuli Pitch lipto-bloliths"- TbAisi, 11Q~,5- PlAll~'i".111i
of Llic Acad Sci Gcorrivai SSR. Acad :,ci Gcovi-inn Inzt of'
ChEmistry imu~td P. G. INclikishvili. (Dirsertationn Cor thc.
Degree of Gancdc4ite of lici(necs)
SO: Knizhneya lctopisl-, No. L~2, 2L Lcumber 19155. 1;'cS(llCW.
DZRAPARIDZI, P.N., DRAXIN, L.A.
------
Production of metallurgical coke from gaseous and weakly-coking
coals. Trudy Inst. met. i gor. dela AN Gruz. SSR no. 8:253-268
'57- (KUU 11:8)
.(Coal)
(Coke)
M"AIMU, kV,; D=RAxl!l LoA.- 1- TVARADZI, L.R,
Investigating Tk1bull tarry liptobiolites for the purpose of
obtaining varnish. Zhur. prikl. khim. 30 no.lltl647-1652 N 157.
(MIRA 1112)
1. roksokhimichookaya laboratorlya Instituta metalla I gornogo dela
AN Gruzinskoy SSR.
(Tkibull-Uptobiolites) (Varnish and varnishing)
RUM, L.A. I
Investigating phenols from generator tare formed during the
gasification of Tkibull resinous liptobioliths. Trudy Inste
met. AN Gruz.SSR 99227-234 '58. (MIRA 12:8)
(Tkibull-Liptobioliths) (Phenol--Testing)
DZHLPARIDZM, P.H.; DIUKIN, L.A.
Some problems in the theory of coking in connection with the
developmant of a now technology for the production of com-
preased metallurgical fusl. Trudy Inst.met. AN Grus.SSR
9:241-253 158. (MIRA 12:8)
(Coal-Carbonization) (Coke)
DZHAPARIDZ3, P.N.; DRA M, L.A.-, DZHINITA, S.I.; TVAR&M, L.R.
Investigating conditions for the preparation of compressed
metallurgical fuel from Tkibult coals. Trudy Inst.net. AN
Gruz.SSR 9:255-262 158. (MIRA 12:8)
(Tkibuli--Coal) (Coke)
DRAKIN L.A ; TVARADZE,, L.R.; IAPIMI N.A.
Coking of Tkibuli coals in-the'~Iarkov rAperimental Plant,
Trudy Inst.prik3..khim.i eL9ktrc)ddm.Aff Gruz.SSR. 3:1&.4-193
162. (MA 16s1)
(Kharkov-Coal-Carbonization)
CZECrIOSLOVAKIA/Chemical Technology - Carbohydrates and Their H.
Processing.
Abs Jour Ref Zhur - Khimlya, No 16) 1958,, 554-17
Author Mincher, Shandera, Drakhovskaya, Shandera
Inst -------------
Title Biological and Technological Prerequisites in the
Production and Quality of Molasses. I. Techmlogical
Methode for Decreasing the quantity and Increasing the
quality of Malasses. 2. Biological Factors Affectiag
the Production of Molasses.
Orig Pub : Listy cukrovarn.., 1958, 74, No 1, 15-21
Abstract : lo A discussion is presented on the theories of basic
problems connected with the production of low quality
molasses (M) in minimm amounts in the sugar and refi-
nery indistries. A theory is presented on the relation-
ship (in M) existing between the saturation coefficient,
good quality, and the concentration.
Card 1/2
CZECHOSLOVAKIA/Chemical Technology - Carbohydrates and Their H.
Processing.
Abs Jour Ref Zhur - Xhimiya., 11o 16) 1958) 55417
The author points out the steps that have been worked
out and utilized by the 14,.-1 Institute of Sugar Indus-
try concerning the innovation in the methods of sugar
and cube oug%r production.
2. A discussion is given on the relationship between
the M quality-and quantity in sugar beets, from the
staadpoint of its quality, the methods for its transDor-
tation and storage, and more particularly, its soluble
ash. Charts are given, showing the relationship between
the amount of M, and from an ash content, and the other
materials (excluding sugar) in raw sugar beets. It is
specifically emphasized that the amount of M obtained
could be decreased by employing a prolonged diffusion and
by using short beet cuttings.
Card 2/2
DRAYIN, L.
Dral~ii , L. - "Methods of' rlcw--lopiny, joint anlral hurnl.,;, (Jiryll,
(Or the retclutior: of thz~ Couricil cif Ylri-'sters USS7.11 an(] cf
thf, ToK VKF(b) on I'Th~, thmu-year plan fox, the do-volop-crt
uf Io-'~ !A lkhoz and so-I.-ho:. PrOCIUCtiV(' IAI)I--:Ial
(l lqll(,, 110.
5,
O'r s '"hurral
SO 1" C, 57), (L, to i,
DRAKINt L. I. eds
Organizatsiya zhivotnovodstva v kolkhozakh (?.%nagement of livestock raising on
collective farmsp ed. by) L. I. Drakin, .11. Yu. Taynkov i L. M. Zalltsman. Moskva,
Sellkhozgiz, 1952.
518 p. illus., diagrs., tables.
At head of titles Trekhletnlye kolkhoznyye agrozootekhnichei3kiye kursy.
N/5
727
.D7
DRAKINt L. I.
BudapeGt - Livestock ExhlbItions
Budnpest Livestock Exposition. Sots. zhiv. 14 No. 8, 1952
I-Ionthl;y List of Rurmlrn Accesclons, Libriry of Con~ress, Novemlhpr 1952. UNCLASSIFIED.
I . I)RAKIN, L.I.
2. IJ33R (6001,
4. Stock and Stockbreeding
7. Livestock at an agricultural exposition in the German Democratic Republic.
Sots.zhiv. 14 no.10, 1952.
9. Monthly List of Russian Accessions, Library of Congress, - January 1953. Unclassified.
1. DRAKIN. L. I.
2. USSR (600)
4. Calves - Diseases
7. Controlled raising of young cattle. Trudy VIZh 20, 1952.
4
9. Monthly List of Russian &qceqsionp, Library of Congress.. March 1953. Unclassified.
1. DMIN, L - 1.
2. ussn. (6oo)
4- Stock and Stockbreeding
7- Controlled rearing of the young is an important method for Im-
proving live3tock, Sots- zhiv, 15, No. 2, 1953-
9. Monthl List of Russian Accessions, Library of Congress, April, -1953, Uncl.
USER/Aryriculture - Stock raising
Card 1/1 Flub. 86 - 7/37
Authors Drakinp L. 1.
Ti t 1e, S ientific methods of developing Live-stock raising
Periodical : Priroda 43/10, 54-57s Oct 1954
Abstract. : Scqnnia description is given of the otock-raining eyJiibit at Un All-Union
Agricultural Fair. Methods of artificial inscm-ination are discussed with
--varticular reference to varieties of sheiip. An .71ccount is ziven of the
success attained in recent ycars in triis work. 'Liustrat-Ions.
InstitLtion :
Submitted :
DRAKIII, L..T.
, ~rp~ko I +
'IF" 7
M
~ search methods in raising calves] Hatodika iosledoyanii po
YyrashchiTaniiu molodniaks krupnogo rogatogo skota. Moskva.
195-5-27 P. (MIRA 10:4)
(Calves)
DRAKIN, L.I., radaktor
[Raising ca Ivan; C collection of scientific papers on methods of
raising calves] Tyroshchivanis molodniaks krupnogo rogatogo skoti;
oboratk nauchnykh robot o astodakh vyroshchivanils molodniaka.
Moskva, Goo. isd-vo selikhos. lit-ry. 1956. 189 P. (MLRA 10:3)
i
lo Moscow# Yeasoyuzu" nsuohno-looledovatellskiy institut shivotno-
Yodetys
1.61TOO)
KIN.- Ioe I nt'Zevlgh.. ISIMSIN, Alekeandr Grigorleyvich;
- 211012-1-773#0 rodakroor; uURIVIGH, M.No, tokhnichaskly roUL-tor
[The *Xommarks" State-Farm] Sovkhoz Ilommunarka.2 Moskys, Gose
ltd-vo sallkhoz.ltt-ry, 1956, 211 p. (KMA 10:3)
(state farms)
DRAKIN ALrgU_jy"Dujnh,_
[Modern theory of acids and bases] Sovremennala teoriia
kislot i osnovanii. Moskvaq Hoek. khimiko-tekhnologich.
in-t im. D.I.14endeleva, 1964. 26 p. (MIRA 17:10)
11,Y6 11 T
U.'.)'SR/Ch eqi s try - Methanes
Chemistry - Benzene
l"47
"Chemical Compounds of Benzene 'Uth lialold-Substituted Vcthnre'll A. F. Knfustinqkly,
S. 1. Drakin ,Moscow Chem Tech Inst imen! D. I. Merdeleyev, ~ Tr
"Izv Aka-l Nauk SSSR, Otd Khim Eauk" No 5p pp 435-42.
Describes study by therimal analysis of sy5ter.:3 consis"Aw- cf 1)~ rzine -Ind cbloro-
and bromo-, anal iodo-substitute4 metbnnes. -ExIst,orce cf hither'V~ ur'known molec-
ular com-founds, some of whicl, wern Is--lated In cr~,.,otalline form,
Ell 53T9
4'tj'~'O 0
Tkfmw "dYlk of
F. Kitpuslistail OW
Own -Tw kwA NO ,
in",
.rw= .. A Adsk
C.Its 40 wo4 plomd It," q tem tube pro.
vul"I 01114 4 lbrilmai'mPlo wm~z=mlll 4 an4
a Otitt" - I hk trof IVbV Ode C: INAk 4114041W lit"IMI
.kb lliciltalm witv. Tile ev " Ill" MV041 in a
3rd tot tulw.' TIW tot tube mote. lbt "OttAt was hw
ak to #1411111% Ow n&L, " trame6a"d back
to OPP- tbom-p-dad. TbeWit-WIrMbW
41 nts cme4parAing t* 111) $4. mA 26 ad,% J
V.11SAM -2hi). -36.051FA 401. rw W4
rutert" at U.7% Cafe and -liV. 17.111 114 404
31v% Cells aml -43.14. end 31.7,r_ M',
5w CJI# and
- 44.4'. This is taken to Indicate file niste"O'l O(CM_
C4114 2CCI,.CJ14. and 3C".C*Hs. Tbt "em Cjh-
CHr, bad a distectic At 50% CeHa and 30.8 -6cs
Poodinx to, WU mWjJqd 2 culft
corers I IS And .6 and - 4.3'.
go,
This arotem form caly Clk.- 14. Thim coavd, was Imo-
Idled. It Conshled of kille prioulatle ce"ale ubkb cvaW
be kept Indefinit'lly to a weaw Container. The avv(am
CA -C14 could not be aludled " dw otbervi because of The
instalmlily of Cl.. Therefore, a bows cla"t" of C&%
WAS Added to C I. in a W*kd it" tww. the hatter Was teml-
nected too a pump and the It" ad C4"# *an file law. Wall
in wt. The othrrolma suWcM Rm bW it break at 00% C~Ifg
Indicatimir Ow possible misteme at Mr4W - TUb mitul"
- - __' - - ~ - - - .-I
carapd. witbout hwOm atudy. xq_ w" C111CU falled
to reveal Its COMP4. W" COO CM "Otme C41"H'j
bad 3 PeTh"de Poinu at 4 "d -60.3* Milil
Cild and -68.91 mad as 392 CO -7'?,4-. TW
m4
rutectit Was at lois COS 107 . Tbw. the a)mtem
NOW Clisch-Cife. 9chamc-4mi. -d 3CICOMCOH4.
lem tompels. w"o leds stable thm Ow a mg CO.
nos. To vhKidate the ntitme W ile' ti oh~
Pd.. "Plo. -ere Made *Ilk
Thil
yWem showed no tnealmls. The fairm4tion of pd.
Olt Tlem C4114-hak~tbanc is altributoble to Me 3 t.-
CM&t n.
9 double bonds In Wfa and to Me dipok mowcav~ of
the C-luslooren bonds to halowthane. The syntheiiied
MUP41- ILIV fTfMtd t0' AS "Cfy5tAll0IPMZ4AAlC% - Tb,
best Offormation olone of them. Clir. CA. W" dall 1t 3 9
M CA. 44, rtwA. %I- II*.h