SCIENTIFIC ABSTRACT ZAGANESCU, F. - ZARGARYAN, S.S.

• Document Type: CREST
• Collection: Scientific Abstracts
• Document Number (FOIA) /ESDN (CREST): CIA-RDP86-00513R001963410013-3
• Release Decision: RIF
• Original Classification: S
• Document Page Count: 100
• Document Creation Date: November 2, 2016
• Document Release Date: March 15, 2001
• Sequence Number: 13
• Publication Date: December 31, 1967
• Content Type: SCIENTIFIC ABSTRACT

Ru mn na
Dtj;mco: Enr-inoor
-riot frivon-
,;oUrc": p Sti-linti si Telmica (Supplenent), 1%'o 1961, pp 6-
lucharcst
D~Itla: "12 April. 1961 O.pened I;p Fabulous Prospects,"

V
CO'Latry:
re-'Orces: En-inoar
Affilicatlio:l: -not riven-
ZOurcQ,,.B
ueharest, Stlinta si Tr,,hnica, No 5t 1961, pp '~2-35.
"Corabina-tion AvIption Engines

SUFLU-13,, Giveln Names
Countrys Rumania
icademic Degreest Engineer Candidate in Technioal Seienoes (Candidat in
Stiinto lehnice).
Affiliations -not given-
gi Tghnlaa -(Supplement) ,-No- 8 0- Aug 1961, pp
Data: "Vostok-21 the Prototype of Pi Iloted Ships-"

88324
HIC02160100010121OW160,-~
(v IN 0 A12!5/AO26
AUTHOM Toodoresou-Tintea, C., Zyag;neacu, Fl., Enginceris
TITLEj Lentioular Aerodynes
PERIODICAL: qtiinV'a 91 Tehnic'a' 1960, No. 12, pp. 20 - 21
TEM, The article deals with lenticular aerodynes and their principle of
Brief-reference is made to the first jet aircraft designed.by the Ru-
manian engineer H. Coand~ in October 1910, and to the advantages of circular wings.
The propulsion and lifting of lentioular aerodynes can be accomplished by the
itCoandi-effeet", which is explained as follows% the jet emitted from the, nozzle
drives Vne partioles of the surrounding medium where no flap is existing and also
the particles of the fluid field located between the jet and t',fie flap. If the J(,,,.
is long en-ough, a depression is produced which deflects the jet in the direction oil
the flap. By using this depression phenomenon, Coandi has defined a new liftine;
method which consists in the production of such a depression on the tipper ;side of
the wing. The lenticular aerodyne is a perfect disc (circular wing) having the
passenger cabin right in the center. Between the edge and the oabin there are four
nozzles, symmetrically arranged on the axes of the wing. By forcing a Jett of ccm-
pressed air or gas through the nozzle, the Coand; effect appears lifting the air-
Card 1/2

83324
11/OC2/60/000/012/002/~03
Lonticul ar Aorodynea A125/A/26
oz-aft. The lenticular aerodyne is equipped with a gyroscope, located in the lower
center of thi wing. Forwm~d flying is accomplished by tilting the aevodynj~, similar
~to the blades of & helicopter. Changes in direction are achieved by modifying th--
Jet pressure. The aerodyne can move in every direction and even hover in thelair.
Finally, the authors mention the utilization possibilities of aerodyne. Share are
6 figures.
Card 2/2

Z.I"'~A!'4','v3r,,U, j Plorin
Given Nares
Cotuit.-(: Rwmania
Acader-Lic Degrees: -Engineer.- Candidate in Technical Sciences (Candidat in
Stiinte To-mice).
Affiliation: -not given-
Source; Bucharest I Stiinta -Ri Tehnica , Vol XIII , No 10 1 Oct 19611 pp 32-33.
Datat '.'Ultrasounds in ftohina Construation."
GFO 961643

TITLE: -The applications- of -cybernetics in space
PERIODICAL: Stiin~a qi Tehnica, no. 12,.1962, 40-41
Starting -vyith -a brief_ slumary of the -points - raised
--by Andrel Prokhorov, 11'ember of the Pres'idium of the Scie-atific
Council for Cybernetics of the USSR Acadqmy of Sciences, on the
applications of cybernetics in space technology, this problem is
described in some detail. The application of electron computers
to the design and launching of space ships,.the training of astro-
nauts in simulated flight patterns within cybernetically controlled
model space ship cabins, and the prelaunching check program perform-
ed automatically by cybernetic circuits on each componew; arA on all
combinations within the actual rockets, as well as the control of
the flight itself, are considered. There-are 4 figures.
Card 1/1

B/002/62/000/008/'002/003
D272/D308
1AUTHOR: __Zdgikeacu.,-P-.l-or4n-t~gineerp- Candidate of Teohnical
Sc~ences
TITLE: -1vostok-31 - 'Vostok-40 in simultaneous flight
PERIODICAL: ~tiin 25t 45
i1a Pi tehnicap no, 8F 1962p 24
TEXT: After a brie-f-presentation of-the intricate technol 'ogical
operation of a rocket launching in its variouri phasest.tho, achiev-
went of-precise launching of a second rocket is examined which rol-
lovis the first 24 hours later in practically the same orb:Lt. 3.ased
on the experience gathered in seven previous satellite laiznchings~
In the -I Coamos '_if3erie.91 it was possible to atthin, 13 hou:rs before
group landingo a difference of 9 seconds in the revolution pciriodn,
of 10 kp in the apogees, of 1 km in the perigees and of 2 minutes
in the inclination angles of the two orbital planes. The various
major-and minor achievnientep-including communication between the
cosmonauts themselvesg and oetween, them and the earthl ar-a enumera-
ted and their importance for future-space launchingsp especj.ally
Card 1/2

R/002/62/006/008/002/003
'Vostok-3' 'Vostok-4l.... D272/D308
in view of constructing launching platforms or scientific observa-
torieq in space is.discussed. There are 3 figures.

WWACI!~y-I=,-.~Srtemi tanar
Traction service achievements of the Rumanian Rau"
and tho perspective of development. KozI tud as 13
no.2:56-65 r 163.
1. Bukareati as temeovari, =szaki egyetemak.

-mig-1 ww ml --,ux 266Vti Immazg-
.134 EgjfT,*
ZAGANESCV, I.0 profol POPESCU, C., conf,
Corrosion action In milroad dieael engines. Rev -milor fer
12 no. It " A 164.

\1
ZAGAVISCU, Ion, prof. .1ng*,4 . Ir1i, cci-,f. tig.; BIRSM , lion,, asist.
Ing, . .
IjHsel engines fov r-;-,' of :-e,0'-,tfhXJ 'Mel;.'. "?R7.
~ I , i .- I"
C-111or fer 12 " -' le- ' ~ 4

ZAGAI~F' T7.F", ing,; '.'alus, ~'Onf. irg.; blIVAN, Ion,
.~Ij `.qpj~ - -'
Asiata Ingo
Diesel engines for secondary lines. Pt. 2. Rev cailor fer
12 no. 4-.r/9-18'1 Ap t64.

ZAGANEWU,, I.
TECHNOLOGY
IMISTA CAILOR FMTE Vol. 6, no. 9# Sept. 1958.
--Modernization of the D2 loomotivep construated at the-Resita Metallurgla
Combinate. p.4119.
J#onthly List of Fast European Accessions (EELI), LG, Vol. 8, No. 34
-He* 1959, Unclass.

T
ZA M. C
Met-hod oif' compjUiv the Pxhaust4 systeyi w-14-.',, bInst pine L-, narm; gwage
lcco.-.,otives. p.192.
-1:117T.F-IJAI
C,%-LOR Fat.TE% (Galle Fernte Rc-mine)
Bucuresti, Rumania
Vol. 7, no. ", kmr. 29"511*
Monthly list of E-,15tern Europenn Accegslon, InOcy (ET-h!) Ir, vol. 0, i;o. 11
November 1959
Uncl.

I-x
Air.

89841
R/002/61/000/005/001/bol
D015 D105
LUTHORt Zdggnoscup F1.9 Engineer
TITLEs Composite aircraft power plants
W
PERIODICAL: ~tiin~g 91 Tehnica, no~ 5, Seria a II-a, 19619 32-33
IEXT: The article deals with aircraft equipped with compoundengines,the main
types of which are enumerated, including a brief description of their advan-
tages. On April 28, 1961.Soviet militaTyli'lot Georgiy Mosolov attaiked an al-
titude of 34,200 m with a "E-661, single-engine turbojet airplane. T~!ntative
conquest of higher altitudes with jet aircraft, such as turbojets, ramjets,
and pulsejets, pregents a problem difficult to solve since combustion, inside
the combustors, lacks the necessary amount of air. Therefore, flights beyond
the atmosphere can only be performed by planes which can carry the n(!cessary
fuel aDd oxidant. These requirements are met by rockets which, in ac:cordance
with the Soviet Scientist Tsiolkovskiy, will be the means used by man in con-
quering space. Since a rocket engine has a high fuel consumption it cannot
power an aircraft over an extended period. The problem is to combine! various
engine types to obtain superior characteristics-within given conditions. In
Card 1/8

8?841,
R/00 61/000/005/001/'001
D015YD105
Composite aircraft power plants
spite-of the-fact-that in 1910, Henri Coandg, a Rumanian scientizt tosted the
-.first jet aircraft, conventional internal-combustion piston engir,es oontinued
in use up to 1945. With turbojets capable of excellent performance at speeds
over 700 km/h and at an altitude of 7,000 _m and with Tupolev's successful de-
velopment of the Tu-104, Tu-110, Tu-114 and Tu-124 it became necessary to mo-
dernize the piston engina. This resulted in the compound engine consisting of
three low-power turbines driven by exhaust gases-connected to the crankshaft.
The turbines are small and the exhaust gases enter each turbine through 3 double
pipes. Each turbine is cooled by a device composed of a cover under which the
air originating from the flight speed flows. A compound engine shown in Fig. 4
rapresents a further step in the development of turboprop engines which are
u;3ed in the "Moskva" IL-18 and the "Rossiya" Tu-114 aircraft. A new type of
engine, the bypass engine which powers the Tu-124 is becoming a rival. of tur -
boprop engines. A ramjet which has an excellent performance at M 3."', at an
altitude of 20-25 km cannotv however, be used for low-speed flights aince
the operation of its engine, having no compressor, :is based on the dyna-
mic pressure of the air. Tho rocket engine fueled by liquid agents does not
Card 2/8

89841
11/002/61/000/005/001/001
D015/1)105
Composite aircraft power plants
have any of the disadvantagps_listed-aboveo,-but eeds-10-15--t -mo e-fuel--------.-
n, imes, r
than a turbojet. It becomes evident therefore, that a composita power plant
incorporating the positive characteristics of-each type of-engime used is
the answer to the demand for high-altitude aircrart. Various p.Dssibilities
of improving the efficiency and assembly of compound engines ha-ve been aug-
gested. One of the possibilities is the fitting of an afterburner to the ram-
jet engine. In such a case? speeds four times the speed of sound can be ob-
tained at altitudes of 5tooo-6toOo m. Another version is the combination of
a ramjet with a rocket engine. The atomized oxygen originating from the com-
bustion products of the rookett which is fueled by concentrated hydrogen
peroxidet enters the combustor of the ramjet where it sup-ports combustion of
the fuels In turbojet-rocket-engine combinations, the tuxbojet engine is used
in the first period of flight subsequent to take-off and in the last period of
descent prior to landing at cruising speed which corresponds to 851% of the
maximum speed. The rocket engine is used to attain high altitude and clim-
bing speed. In some cases, the rocket engine is 1he main power plant. In t/
Card 3/8

89841
it/002/61/000/005/001/001
D015/1)105
.Composite aircraft power plants 1X,
-such- cases the. aircraft is -equipped -with a--multi-combusto.r. engi:.'Ie_ to obtain
a constant thrust. The tips of aircraft wings are equipped with low-power
turbojet engines which insure the flight at cruising speed. Tha main advan-
tage of such a combination consists in insuring high maneuverabLlity and high
speed* The rocket engine used as main power plant, howevert ha3 the disad-
vantage of reduced action radius of the aircraft. Data on a new type of en-
gine, the turbo-rocket, are being published with 1peater frequency. This type
consists of a combination of a rocket and a turbojet engine. In spite of con-
-siderable difficulties which arise in the design and construction of composite
aircraft power plants, the author believes that such plants will play an im-
portant part. There are 5 sketches.
Card 4/8

,Composite aircraft power plants
Fig. 1. Experimental supersonic
aircraft in which the power plant
is a combination of turbojet and rocket
engine@
Fig. 1.
6984
R/002/61/000/005/001/'001
D015/D105
Card 5/8

89841
R/002/61/000/005/001/bol
D015/D105
Composite afroraft power plants
Fig. 2. Supersonic aircraft with a composite turbojet and ramjet ene-ine.
Legend: (1) Valves, (2) Ramjet. (3) Turbojet, (4) Diffuser, (5) Re-
serve tank.
Fig. 2.
Card 6/8
0.0
4

69841
R/002/61/000/005/001/'001
D015/DlO5
Composite aircraft power plants
Fig. 3. Scheme of an experimental.aircraft with a turbojet and ramjet engine.
Legendt (1) Cabin. (21) Fuel. (3).,Ramjet. (4) Turbojet. (5) Shock.-wave
breaker.
Fig- 3-
lop.%
VP
Card 7/a

89841
R/002/6:L/000/00'5/001/001
D015/DlO5
Composite aircraft power pl&nts
Fig- 4. Turbocompound engines
Fig. 4..

furbaCOMP4444

C ard 8/8

10 (7290)
10 6
it IJI,112 -11 -1 - G /it 3
AUTHOR: Wgdnescu, Florin, Engineer
TITLE: Flight at ~-yp-ers-c-n-ic Speeds (Zborul cu viteze hiper-
son ce
PERIODICAL: tiin~i~[ gi Tehnic A 1959, Seria a II-a, Vol 11,
fir 1, pp 11 - 13 ?RUM)
ABSTRACT: The author mentions statements of academicians L. Se-
dov and A. Nesmeyanov-that "the time when manned space
ships will be sent on,interplanetary flights is not
,f,'Lr off" and "the solution of various problems such as
the creation of permanent, controlled satellites,
their return journey to the Earth, and rocket fligiats
to the Moon and the nearest planets, is a part of the
program of USSR astronautical research activities for
the near future". Stable hypersonic aerodynamic flight
could be achieved within a "corridor", the upper 11-
mit of which would be determined by a zone aithin
Card 1/4 which weight would be equaled by the bearing force

RUZJ/2-11-1-6/43
Flight at Hypersonic Sppeds
plus the traction force, and extend up to the prima:~y
cosmic speed (8 Icm per second). The lower limit of
the corridor would be limited by a zone within W'i-.h
friction temperature attains ap-proximately 1,0'.0
ohich is the maximum tolerated by the skin of the
flying body. To solve the problem of hypersonic
flight, including safe landing on the earth's
surface, the corridor vould have to be extended. by
devising adequate trajectories and by using malt.%erials
that are highly resistant to very high teraperatures.
Ballistic rockets fly at very high speeds and C;reat
altitudes; t1iuss, a ballistic rocket having an c.ction
radius of 9,650 Im, reaches 7.16 kps and a-,tains an
altitude of 1,320 I=. Other ty-pes of hypersonic
craft with h-iP-,h-act-*Lon radius are: the ricocheting
rocket, and the -.-rin-ed glider rocket which was design-
ated as "rocII--et-Mlane" by Soviet encE-ineer Aleksandrov.
Card 2/4 The latter consists of the second stage of a two-

RUL:/2-11-1-6/43
Flight at Hypersonic Speeds
stage rocket,-and-has an empennage-i-n-addition. to the
wings. The first stage would boost the rocket to
altitudes of 500 to 600 km .,.,here the rocket glider
could attain the first cosmic speed. The rocket
glider carries sufficient poaer reserves to bteak
away from its orbit and return to earth in a gliding
flight on a tangential trajectory after the wing sur-
face has been modified. The ricocheting rocket con- F
sists of the top stage of a multi-stage ballistic
rocket and uses the ricocheting effect within the
dense strata of the atmosDhere to increase its action

present, however, the winged rocket glidor seems to
-be _the__only__ acceptable hypersonic; -vehicle-since - it
--
-can be guided during its descent trajectory, which
makes it possible to select a return route with
minimum aerodynamic heat. Uhis fact is Lmportant
Card 3/4 since this type of rocket attains speeds up to
w"I 3L -kiakhii
___qM -IFXP- N_
RE f~~'_KV "WHIM"Mr- 9'. MW= ME FEIN,
10-0 - - z V - -, '

g !b

RUM/2-11-1-6/43
Flight at Hypersonic Speeds
16,000 kph at altitudes around 40 km. The author
describes Vao possible future types of hypersonic
craft. The hypersonic glider consists of a Uxee-
stage rocket, the top stage of which has a large-
angle, arrovi-shaped wing. It can leave its orbit and
return to earth. It would be manned by a crevr of
five. Its total weight would be 4150 t2ns, and. the
load.on the wings would be 54 kg per m . The other
type is a so-called cosmic disk to be used for inter-
planetary f light, which would re-enter the atmo-
sphere on a tangential trajectory with minimunt aero-
-dyna.mielleat.-_
Card 4/4

29(l)
AUTHOR: Z6g6nascu, Fl., Engineer
TITLE: Millions of Horsepower
PERIODICAL: Stiin~L ~i Tehnici~,- )Seria a II-a, Vol 11, Nr 9,
A
Oupplement, p 2, col (RUM)
ABSTRACT: -Brieflymentioning the-Soviet- arti~ficial-satellitos
and space rockets, the au`~-.hor de9cribe;3 the modus
operandi of a liquid-fueled rocket engine. He also
t4StS
assumes that Soviet scien . used for the second
--oket _higha-iwqlity chemical~fuelj abl;e-to-de-
Space ro 'I _L
volop an exhaust speed of over 3 11; rautt also
have used high-quality heat-resistant nateri.a1c, Con-
sidering that the lost Soviet space rocket consisted
of 4 sta-es, the weight of the fuel per stage repre-
seated an average of 80yo of the total weight of' the
respectiva stage.. The remaining 20% included the frame
stz~ucture, engines, fuel tanks, auxiliary installations,
etc. Also considering that the rocket was pxopolled by
Card 1/3 AL-1s giving an exhaust speed of over 3 km/sec, and

----- - - - - -
Millions of Horzepower RULT/2 -11 -9-40/42
~e we i gh ed
t tal S tart-ing ae-16hill- of' .100 ton,,: - - the- last- star
-ibuz; the -winC; 2 possi-
7 tons. The author desci , follo
bill-ties, IL to tal t 100 tor'.;~~,; nwnber of stagess
4; sta6e I "~5 tonj --tago 11 tons ; i3tagc, III.
13 tons stage IV '-'cns e;dhaust ,ielocitullr - 17i, I
i 3:- of Stu-'3s:
kiVsee d '2" )' t o t a - 1 %1; ei:j 1 t -100 tonz; numbs. C)
4; sst,):-~,e r,() tons; s,1,--;,e Il - 2! tons-, st~iae III
12 ton-, ; 0 ta-u-'2 IV ton..; ; ex-hl-iaslu- velocity
ma:! J. '01
P:in/ s e c U s in G th~, ~ __-, -_~'Jo formula given by Tsiol-
hovsk-l-LY1 the parti_ul and finrA. pfl-rformlance of a --ocket
similar to the rochets uoed on 2 January and 12 Sep-
tember can be d,-_~'Ucrmincd. Their values are shwar, by
the Onclos,-d table, These 2 tocl,~ots could have been
used for launchin- a 6-ton oatellite- The s,~ccjnd
possibility su'pplles a 'Lanal speed of 1-1.22 km1sec,
,;hich ~s vc -f close -G ~-h(:., real. value. The adv-3ntage
1 01 11 1
of la--e a_-tifici_~;! satolliteS 'Lor future Moon trips
is .,,,ell known Alroadly an -'_nitial speed of
8 1,-n/soc, the roc"'e-t- only necdj a boost of 17..2 km1sec
to reach th,~ llooln Uz;inc a chemcall fue! which develops
2/3 ait exhaust; sp,,-.~ed of th-e rocket only need

Millions of llorsepovrcr
10 tonf, of fucl tri OTeilcome arth's gravitational
tons derdwoigh,-- It is
1 11 1. t ") n p y J, - r) - ,i' !~,n -
f,ossiblc to ~;u-rid a unmanned rocket
A ph( tograpli the Moon I o
to th~,, ~',oon. vihi.ch woul.~-]. fir-t,
,,surface and' ~',heri ve-Aurn 'U-(-) Uiu or or,blt'the
Moon a:~ a -latt.,11ite. A 6,00-ton, )-,tag5c manned Moon-
vocket would c.--; 'i,ry a ziov" of 4 and I ton paylbad
moving on a trLms~,-,r orb-," to bisect the ei.-~ular or-
bits of the E,,-lr4.-h an-ra' t-he l'i'loon. The 2-1? cn,,-ines -vitould
u--c che:.%icul fu r- 1, oC bor-on _-lnd fluorine, and
the last S'--a-e vmuld- v;ei.,gh 1'-.0 tons v,,he--, sta.c-tin3 back
u 0 -
from the Moon. Therc _i-- I table-
Card 3/3

ZAGARESCU,, X.; SALCEANU, C.
Experimental study an the elastic extension of metallic wires* P. 75
Academia Republicii Populare Romine.- Bata de Cercetari Stiintificoto_
Timisoara. STUDII $1 CERCETMU STIINTIFICE. SERIA It STIINTE KAVEHATICE0
FIZICE, CHIMICE S1 TEHNTCE. -
Vol. 2, No. 1/4, Jan./Dec. 1955
Timisoara, Rumania
SOURCE: FAtk-t Ravapean List (EUL) Library of
Congress, Vol. 6. No. 1. January 1957

UGANSSCV. M.
Assoolated oporstors of multipositional olownte, Comunicarils
AR 12 no.5019-54 Yq 162.
1,4minicare presentata do aoadwdoian Gr. 0. Vbisil,

Mihai
SURNMIE, Giveft- N#Aes
Countrys Rumania
Academic Degreast -Engineer-
Affiliations -not given-
Sources. Bucharest, Stiinta, pi Tehnicat Vol XIII, Wo 129 Deo 1961t pp 14-15
Datai"The Moseow-Baical. Main Railway Line."
Gov)

M
7.AGANESCUp M.
A-Ceneralization of-dlapersion-relations. Studil fiz--tebn Iasi 13
no.2:171-174 160.
(Particle size determination) (Q=t= theor7)

ZAOANESCU Me
--saso-new properties of the Dirae-bilinear-forms.-fitudii com-fiz
iLno.z.5Zl-528 160. (13W 1W)
1. Inatitutul pedagogic Timisoara*
(Forms (Mathematics)) (Potentialp Theory of)
(Harmonic functions) (Particles)

n de I'sg!" C
R CIC N,
om,ne. Bul. . . ITiz.
8 (1956), 715-722. (Romaniaq. Rusiian md Freach
susnuttaries)
"On montre qu'un sch6ma correct de I'Pspacc-temp~
qttarttifi6 rte firut iftre qb'cenu A I'ca qumitific cu plms
Bile witre grandeur xjul P-cut ~trv interpmWe comme la
~me courdminde spatio-turporeUp. Lc r&emi 5-
cinquit-
Aimensionnel e~t invariant par rapffort & tin cutain
groupe de rola.tioni de 1'espace k 5 dimensions. 'Dans le
cas le plus siniple, tridimendrinnel, ce groupc cit hamo~
:A du groupe mililaire, conriti de It (b&,rie In
7: func6inq elliptiqu es.
7,. i
Dans 1e cu du ranuven-ent de Votectron dans tin champ
.6le-dromaguiltiqne a un champ gravitationnel, (in pcut
Prendre le temps propre comtre 5 crxrdortn6c. U qLartti-
fic. -;s propre rku,-- A une i6quation de rnouve-
i(ion du ftnil
ment analague & celle qu'on obtiont de ft thbric. du
champ auxiliaino." (RcsumiS de Pautcur.)
A. G. iValker (Liver"il)

7:-,Ysics T.,=y .3 1
~-d FIA -2
ALs Jour 7;.ur - Fizilm., Ilo 5, lq5gl uo 9,3o1
Au ;: or : Za~;ancpcu '.i.
Lis L : Facvl'u,y r)-
'5" a "ia"t"Qrial. I --I~ ill
OriG Anit. -V--. ysik; 195a) ij No 6-5, 424-428
Abstract Rilativistic :iTiation-3 r)f' a ~ atrinl poin'~. ar,-, d,:Scri,.j,:d in
v,Aocity snac t'--u
11 ral cquation :iodo,-,rnlh is
ar casc of pla-,IQ 1 .0tion ur-,,!,-,r -t*-
0 'I"lin'.x4. a -,!.,lrtic,,LIL
ol a cons-Lant L'arcc is L;xa.-ILI~A. Ya.I. Il-Li,-ac-l-w
Card 1/1

TOLKOBOT M.F., prof. -_ZK_ASXLVL,-" (Zabanledlo,, V.0.1; MAA, N.G.
tKoksha,.N.H.1; KIISLITSKIY,, Ya.P. (Kyslytalkyij IA.P.]
Using Aeat indust,-y uastes for the production of foads. Khar.prou.
no.055-59 O-D 162. (MIRA 16:1)
-1. Ukrainakiy nauchno-issladovatoallakiy institut wyamomoloobnoy
proVablannosti Gooplana UkrSSR,
(Feeds)

-A -ky - - - JDW44-G.
A IR~TT uke)
034355 SOURCE CODE1 UR/0000/66/ooo/ooo/oll4/ol2l
AUTHORs Sandulova, A.-V Marlyamova. r. I.; "a auXach, Yu. I.
ORGt L'vov Polytechnical Institute Wvovskly politekhnicheekly
Institut
TITLE: Piezoresistance properties of acirular and filamentary single
crystals ,p f silicon
SOURCE: AN UkrSSR* Poluprovodaikovaya tekhni.ka i ml.kroelektronika
(Semiconductor engineering and microelectronics), Kiev, Maukova dumkat
1966t 114-121
TOPIC TAGS: strain gage, pressure transducer, piezoelectric crystal,
piezoresistance effect
ABSTRACT: The piezoresistance properties of acicular and filamentary
single cryst Is of silicon vere Investigate4o The crystals were grown
fro silicon-in the presence of Br*,Iaolvent; p-type crystals
were obtained by Br and Al doping and nZWype, by An doping. The
contacts vere made by welding gold, silver, or platinum m! 'crowire
(20 to 100 u) to the end of the crystals. To produce tencile or com-
preasive strain in the sample, it was glued to the u 'pper ar lower Sur-
face of a beam which was periodically bent (in the vertice.1 plane) by
Card 1/2

-L-0843o--67
ACC NRs AT6034355
a special device. The precisely measured bean deflection vas used for
I
lt~
calculation of strai Nin the sample.,tThe resistance variation of the
samples vas measured using an MOD__58 d-c- bridge~together with an
EPP-09-Ml recording potentiometer. The strmi to-resLotance relation
is linear for both types of crystal and both types of strain in the
.1.10-4_8.10-4 strain variatio'n range. High-output signals (40-80 mv)
from this crystal can be-recorded vithout amplification. The sensitiv-
-ity -of-the p--type crystal sensor is 50-70 timei higher than that of
Fdtallic crystal sensors. The sensitivity of n-type crystals is lov,
Orig. art, has; 2 formulas and 8 figures.
1.70
SUB CODEt 099 SUBM DATE: Dec64/ ORIGREFt 003/ OTH REIF: 012/
ATD PRESS: 5103
2t2

Or[:anizatlorxi and It"asks. -)f staffs in forest.rY. P. 12:54
(7veza (Iru&tr,,v in-,criArlev In Lelmlkt~lv
~Jubljana., rugoslainia, Vol, 10, no. 2, I.Ipr. 1951).
-cnth2 -14st of the ;bast 2-iirr~pcan -,,ccosic~ s Vol.. 8,
Y (KFAJ) LCI
U

FUKARAK, P.- IWAPRO J.; YES11"ROVIC, S.; KIEPAC, D,; LHETIICEK, Z.i MIJANAC, D.;
SEVNIK# F.;.,-ZAQAlR,,.D~; MIKLAVZIC, J.; KtffZt A.; PIPAN, ft.; FUNKLt L.;
SVETLICIC, A.; ZUMFR, L.; KE700 it.
Revoiw of periodicals; silviculture. i3ul sc Youg 9 no.4/5:144-
145 Ag-0 164.

ZAGAR, Cirilq in rof, (Ljubljanat Vegova ulica 4)
The vacuum impregnation of transformers. Elaktr vast 27 no.11/12.-
375-376 N-D '59- (ESAI 10:1)
(Ele6cric transformers) (Vacuum)

ZAGAR, Damir, inz.
Influence of temperature ax! pressure on the absorption
process in the caoing-heae gas at the Klootar Gas PlAnt.
Nafta Jug 23 no. 11/12:427-434 11-D 162.
1. VeLf taplin, Zagreb.

ZAGAR,, Damirj, inz.
Influence- of- temperature -and -pressure 3-the adsorption -pr Dwca----
Jug 13 no.n/12,
casing-head gas at the Klostar Gas Pli * FAtta
427-434 " 162.
1, Naftaplin., Zagreb*

. ZAGARL Pmc,_inz,
1ugoslav# Is a solid accuo-mic entity. Automtilra 3 no.6:-M
D 162.

Fy. A A 6, 1 0 IF:, 2m~ T !FZ4 15 V R ~4 -,4Tiv 'r
UA G- MR, M.,
GMULUTY GEOLOGY
ZAGAR, It. Geoirnphy of the burg of SentJur- p. 263. Vol. 27/281
1955/56 (published 1957).
Monthly List of East European Accessions (EEAI) Vol. 11, Vo. 2.
April 1959 Unclass.

now antimlig.1-OtIC mine.' 533.
(GLASNIK, Vol. 5, No. 7, ~iejy 1957)
SO: Monthly Uat of East European Accossions (FEAL) Lr, Vol. 6v iio. 12, Dec. 1957
Uncl.

7AGAR P.
"A new anti-infantry fragzmantation Yrdneoff
p. 835 (Vojno-Tehnicki Glasnik) Vol, 5,, no. 3-1, Na7. 1957
Belgrade, Yugoslavia
SO%*., Monthly Index of East European Acconsions (EEAi) rc. '701. 7,, no. 4,
April 195 8

ZAGAR I Z. . -
Antibiogram. Lijeen. vJeam. 84 no,6s589-590 162.
(ANTIBIOTICS phairacol)

Krunoslaval SKALOVA,-Rddm1la; ZMAR0 Zivojin; LAIRCIG Rankal
TOMIC-MMIC ' I I
VCDOPIJis Alemka
The problem and appearance of resistanco strains of Stkpbylococcus
pyogenes. Rad, mod. fak. Zagreb 8 no.lr5-25 160.
(STAPHYLOCOCCUS col)- -(ANTIBIOTICS pharmacol)

ZAGAR, Zvoolpirh Inzo
From the activities of ths Society of Corwtrllctiou Engineern and
T*elmioians of Croatia* Gradovinar 15 no*202-66 Fe 163.
1
I

.,,;ivojint dr.
Bacteriological examin4tion of qmtun vith apecial referonce
to the patbogenic role of the moat-frequantly ioolated mioro-
organi=3. Lijecn. vjesn. 85 no.0409-414 163-
1. -Iz odje-la za bakteriologiju i perasitologiju Skole narlxlnog
zdmvlja NA. Stampar" Medicinekog fakulteta u Zagre.,bu.
(SPUTMO (STAPMOCOCCUS)
(STREPTOCOCCUS-PYOGENES) (EMSEELLA)
9AEMOPHILUS) (HORAXELLA)
SCHERICHIA COLI)
N

ZAGAR. Zivolin.,dr
Now antibiotics and their uw In human mdicine. - I%d.- glats. - Iw.
12/l2at428-433 D 16.1.
1. 0djel za baktariologiju I parealtolog1ju Skole- narodnog- zdmvlja
"A. Stampar" Medicinakog fakulteta Sveucillsta u Zagrebu.
(ANTIBIOTICS ther)

ZAGAP Z.
Clinico-bacterialogical aspeCts of cbronic "Droncbitio,
Lijecn. vjesn. 87 no.2-209-211 F 165-

S~IUGO'~CLAXIA.
ZAGA2, Dr Zivojin, Departriient of 13actcrioloGy and x1arasitol-
'--b--n-i"Dd'JVT--Z-a--P-Plcterioloeiju i darazitologiju), A,, btaml.,ar.
Public 11calt'll ScIlool (SI-ola Jarodnog Zdravljt% "A. L)tum-
rar")s Fnculty of Mledicine (1-ledicinski Yakultet), Z,4(yreb.
IlThe Bacteriolo-ical Examination of Sputum in the L:'4ht of
0
the Pathogenic 11ole of the Microorganisms Most Cczxwnly
Isolated."
Zaglreb, Lijecnicki Uesnik, Vol 85, Ao 411, April 196Z~, Ap
409-414.
Abstract: ZKu thor I r3 L ngi i eh nu=rary modif ie d7 The au thor a
discuss the problcm of sputum sEunpling cand the bacteriolog-
ical examination of such sw-,-plesl us well as the interpre-
tation of the bacterloloj;lcal rooultae'.Ahe mosit, common
bacteria of the respiratory tract are divided into three
groups, Viz., rredominantly rathogenic, predominantly
r.otentially pa~hoeenicj and rredominantly apathogenic.
L/l/Table, 23 Western and Yugoelavreferences,

ZAGAR,ZivojI-n,ttr.; UGRC 10, Iran&, dr.
Analysis of the r6sistance of staphyoloocat during the last four
years. Had. glean; 13 n0-7:360-363 J1 "59.
1. Zavod za mikrobiologiju i parasitologiju Skole twirodnog zdravlja
OAndrija Stam.par* Medicinskog fakultata u Zagrebu, I.."redstojalk:
prof. dr Dora Filipovic.
(STAPHYWCOCC'US pharmcoIj
(ANTIBIOTIGS pharmcol.)

JUNG, M.; CMCO Jets-ZAGAR,-Z~
Preservation of live pathogenic bacteria dried in vacuum in a low
temperaturoo Hi jena,.Beogr*.l2-no*2/3i226-230 160,,
(BACTEMIi- -

UGAR, zivojin, dr,
laboratory investigations and principles for the clinical. use of
nitrofurantoin. JAjacn. vjesn. 94 no,4:3394-3" 162,
is-, Xx0djela _za,__b%kterIologIju_I_ pamaitologiju- -Skala narednog zdmvlja
"A. Stampar" Medicinskog fakulteta u Zagrebu.
(NITROFURANS ther)

ZA'W.
Y',aga-riziskaya, L. A "-'nve: t' of the r.., th%-, r, -
ac-d cill", trudy
So: 10 April. 53, (Lntopi:3 lZhurnal %'A~itpy, No. 12, 19.1,9).

BEW-11, Boris Ivanovjch.--.WARIV=YA.-LyqdmIl& laekoemdrovna; VAM JFA.
takha. red.
ALIKSANDROf, J
[Printing materiald Policrafichaskis materinly. Moskva, 405.
izd-vo Olskusetvo.0 1953. 618 p. (KIEA 120)
(Printing nachInery and supplies)
(Bookbinding-Rquipment an& supplies)

f
YNS HWWO, V dim r &Ymovich, inzh.; POTMKIN# Dmitrty Mikhaylovich, kand.
teldhrnauk; ZAGARMKATA, I.A.. re,teentgat; LUKOV, I.A., nauchW
red.; MUKNIN, M.T.. takha.red.
[Cardigan stitch and reversible machines anti the tecbnolooKr of
weaving outer garments] Fangovye i oborotaye mashiny i tekqnologiia
varkhnego trikotazha. Moskva. Goe.nauchno-takhnoisd-vo lit-ry po
legkol promyshl., 1958. 408 p. (MIRA 11:5)
(Knitting machines)

DlDERKOp K.I., kand. tekhn. nauk; C-AFAMOVICH, M.D.; ZAGART~j G.1-11 ARTGOV,
Yu.Oe-; SHRAMKOP X.R.
Electric regulator of a ferrodynamic system. Art* I prib. no.4:
64-66 o-D 164 (141R& 18:2)

VASILIYEV, V.G.; IVXT0Vp A.P.; VCSTRYAKOV, 0.1.; SHMITELISKTY, 1F.N.;
GAPANOWCH, M.D.; DIMINO., K.I.; ABUGOV, Yu,Ol SHRAHKO, K.N.;
ZAWIY,,G.1,; DUDCHWKC-DUDKO, V.M.; HIKULIN, Yu*Ta.;
4'u-".N.; BYKOVp VA.
Inventions. Avt. i prib. no-4173-74 O-D 164 (MIRA 18t2)

Add NR,
-"7001824-- --SOURCECODS: AR/0119166/000/012/0012/0014
jAU111OR: Abugov,.Yus Op (Engineer); Gafanovich, H. D., (Enginear); 2agarly",J.,
(Ensine6r); Shramko, K. N. (Engineer); Didenko, K. 1. (Candidate of technical science
ORG: none
TITLE: Proportional-plus-integral regulator with nonlinear integrating action
SOURCE$` Priborostroyeniye, no. 12, 1966,-12-14
TOPIC TAGS: nonlinear control system A-Avatiol
ABSTRACT:_-A proportional-plus-integral.regulator serially producedisince 1965 is
described in which the duration of integration in Inversely rolated to the magnitude
of the error signal. The block diagram of the regulator (see Fig. 1) has an analog
r
f
r X*
Xi J4
It
Fig. 1. Nonlinear proportional-plus-
+
+ integral regulator4
Card 112. UDC; 621,39078

J(& NR. AP7001824
'Oropo'rtional-, b r4nch-_ (I)-- and --a- diacrate -integral. -branch.-which --cdaa to oof ~4~pulmi
width modulator with coarse quantization (2) and an integrating reluctance motor (3)
in addition to a unit which establiehes the integration time. The integrator speeds
up integration time considerably if the error signal exceeds 10%. Ilius if errox is
in the ranges 10 t x & 20%, 2 f. x < .10%, and 0.5 1 x < 2% of the maiLimum signaI,
integration ti
me is correspondingly reduced by 4, 8, and 16 timen in.comparison
to.rhe integration time corresponding to x > 20%. Regulation time io 1.6-2 times
less than
''that required by the-linear proportional-plus-integral regulator. The
transient process lasts approximately 80 sec as compared to 1300 see for the linear
regulator. The regulator characteristics are: range of gain adjustment, 0.1-50;
range of integration time variation, 20-20,060 see; Input and outpul: signals, both
0-2 V, to 5b~pu, weight$ approximately 12 kg; and sizes 280 x 164 x 220 m, Allowable
temperature and-humidity ranges are 0-50C and up to 80% rdspectively. Orig. art.
has: -13-formulas and 7-figureso JBDI
SUB-CODE1, 09/ SUBH DATE: none/ ORIG REPt 001/ M REFs 001/.
ATD pREsS: 5116

ZAGARIY L B.; KARDONSKIYj V.M*
.-Tranamittod bean in the case of anomalous Uray abcorptiono
Kristallograftia. 8 no.2s263-264 Mr-Ap 163. (MIRA 17 18)
-1. Institut metallovedeniya-i fiziki- metallov ISentralInqjo
nauchno-iseledovatellskogo instituta chernoy matallurgii Imeni
Bardina.

ZAGARMISTRp A. M. 11
Zagarmistr,-A. M. "Electric depth sounding," Prild. geoflzika, 5,
.1
1948, p. 54-72
SO: U-3642 10 AprII, 1953 (Letods 'Zhurnal 'nykh Statoy, no.e,, 1949)

Sr
lqrr~RIAIW 15, -
RVZNIK, A.K* (bripdir), ARIST, M., BLOKH. I.M.. KIKGM. %.A.,
ZAGARHISTR, A.M., KUPAWY-TAROPOLK, I.X.,-PSTROT, L.T., TTABIN, T.Ys,
-NDMOMM. -A.M., sostaviteli; DYUKOV, A.I., IUSHCEMV, A.L., redaktory.
(All-Union unif tod-norms for-geophysical f 161d work), IsesoLusn"
adinye normy vyrabotht a& polevye geofrafisheekle raboty. [*.SOStaTi-
tali: Resnik A.M. L dr. Radaktory: A.I.Diukov. A.I.Slashchtiv] i(0_
skva, Go*. nauchno-tekhn. izd-vo neftianoi 1. gorno-toplivuot lit-ry,
ig5l. 146 p. (MMA, 7:4)
(Geophyalce)

Z A 6R t, n i z - CA+ ~ Ar)
"0v, TaygerAy Nikolayevich; SO. 3-m-Ae red.; Ms IRA, To.T..
vedushchly red,,- POMIN takhn. red,
slactria.- logging, graphs]. -- rntoiTntatslla,---
krivykh vertikallnogo tloktrichookogo toudirovantla. Nosimi, Goo.
nauabno-takhn, lzd-vo ueft, I 90=0-toPlivu0i lit-rY, 1957.. 1+71 P.
(Mosoov, Yvecoluzmyl u=chno-Ismledom%el'xl:ll lustitut elpfisiche
sK.kh motodov mzvedki. ftudy, no.1). liclu lirl)
(Pro"atitig-aeophysical -vathods)

ZAGAIN 5
Utilization of Increased-resolutiou d1pole-axial soundIng In
probiv4g 3-tn)e arose sections. Pr1kl. goofis. no.16-.130-144
(KLRA
(Prospecting-Geophysical methods)

- - r,
I-R-- -- - --
ZAGARMISTR, A.M. ~ -~ .: .
- -
---- -.-- Rvaluation-of tho-- screenirg- effect of -hIgh-resistance strs.ta In - - -- -
vertical electrical prospecting. Prikl.gooflz. no.17-.147-1-31 157.
(mllu 11: 2)
(Prospecting-Geophysical methods)

ALIMYET# AaXe; BMICMffSKIY# X*K*; WARMTH &#if
Use of now methods In elaotrlo prospectlag b8lberiat Prii:l. geofix.
uo;18:103-127 158 (MIR& 11-5)
(;iberia-Prospeoting-05o:pbysicaI methals)

PHASE I BOOK EXPLOITATION 1031
Prikladnaya geofizika; sbornik statey vyp. 19 (Applied 1'eophysic!3;
Collection-of Articles, Nr, 19) M;scow, Gostoptekhizdaot, 1958.
253 p. 3,000 copies printed.
Sponsoring Agency: Vaesoyuznyy nauchno-isoledovatel'skiy institut
geofizicheakikh metodov razvedki
Ed. Bogdanov, A.I.; Executive Rd.: Dobrynina, N.P.; Tech. Ed.:
Polosina,- A.S.
PURPOSE: This collection of articles is intended for professional
geophysicists'engaged in scientific research or working in indus-
trial enterprises.
COVERAGE: The articles are devoted to a discussion of methods of in-
terpreting various types of electrical logs, methods of determining
the porosity, permeabilityand specific surface characteristics
Card 1/4

Applied Geophysics (Cont.) 1031
of water bearing rocks, and methods of determining the physical.
properties-of-sediments and-the characteristics of-varLous phy---
sical parameters. A description of piezoelectric presisure re-
corders used in seismic exploration is also eiven. The articles
are accompanied by graphs, tables, and bibliographic referenceea.
TABLE OF CONTENTS:
Rudakovskiy,GJ._, Zverev,_-S.M. Piezo-crystalline Pressurd-Recorders
in [Off-Shorel-Seismic Exploratio 3
Al'pin, L.M. Transformation of Eleqtro-logging Curves 23
Zavadskaya, T.N. Notes on the Transfotmation of Ele.c.tro-logging
Curves 47
Berdichevskiy, M.N,, Zagarmistr A M Problems in I-terpreting
Multi-Stage Electric-a To-Ws-_I_;_'hI _~i;;le Installations 57
Card 2/4

Applied Geophysics (Cont.) 1031
Faradzhev, A.S. Investigating the Effects of Non-horizontal Plane
Boundaries on Electro-logs 109
Shapiro, D.A. Discussion of Theoretical Problems on Diffucion-
adsorption Potentials (Diaphragms) in Boreholes 129
Morozov, G.S. Methods of-Determining Porosity, Permeability and
Specific Resistivity per Unit Area of Water Conducting.Suffaces'
from Electro-log Data 170
Keyvsar, Z.1. Relationship Between Relative Resistivity., Porosity,
Permeability and Specific Surface 1116
Avchyan, G.M. Determining Magnetic Susceptibility with Dolginov's
Astatic Magnetometer 195
Kalinina, R.V. The Correlation Between the Velocity of Propaga-
tion of Elastic Waves and the Relative Elastic Constants of Rccks 216
Card 3/4

Applied Geophysics (Cont.) 1031
Filippov, Ye.M. Investigation of the Diffused Spectrum of Gauma
Radiation in-Rocks of Different Mineralogical Composition and
Densities 230
Veselov, K.Ye. Golomb, V.E., Kalisheva,L.V,, Kudymov, B.Ya.,
Lozinskaya, A.I. Review of P.I. Lukavchenko's "Gravimetric Ex-
ploration for Oil and Gas" 245
AVAILABLE: Library of Congress
Card 4/4 mm/sEm
1-22-59

BLOKH, I.H.; 94 IM. A.K.,- FARADZHU, A.S,
Guard electrode method and Its use In n%pping coal.seem.
-RaimMo I -oMsnedr 24 - no.10,.34-39 0 '58. (NBA 1212)
Vessoyuxnyy nauchno-issladovatel'skiy ugollnyy institut
(f or Blokh) 2. VeeeoyuzW , w hno-lealedovatel I sidy inst Itut
6pof1x1k:L (for Zagarmistr, ftradshav)e
(Prospecting--Geophysical methods) (Coal,esology-Raps)

%AaARRISTR. A-M-; HWICHKVSXIY, M-N-
---4hlng-the talluric current nothod in electric prospecting. Geal.
naftl I gas& 3 no-1:3&47 Ja 159. (MIRA 12:4)
1. V8680yusnyy nauchno-issladovatallakly inst1tut Goofivikas
(Prospecting) (Blectric currents)

U-G&MISTR. A.M.; FARAZMV.. A.S.
---Utio;-Ct-th:eee-.!elAictrode-appamtus mith a-ishie]Aed-eleetrodAi-in-mappinf,,
conductive coal-se=a. Razved. i ol:ho nedr 26 noj'-35-38 AP
highly
160. I.ICIW. 15:7)
1. Vseoayuznyy nauchno-issledovatel'aldy Institut, geofizl'.cheskikh
metodov ragrvadkia -
(Coal geology-Hapa)
(Electric prospecting-Equipmet, amd supplies)

ZAGARMIS TR A, M. de cea&edV VA-141YAN, LL.; KOROL'KGII, Yu.S., 7EPMUN, Ye.l.
Electric prospecting b7 the field produotion method. Izy. vys.
ucheb. zav.; geol. i razv. 6 no.9;1.20-132 S 163.
(MM 17tlO)
1. Novooibirokiy Inatitut geologii i goofiviki Sibi:rskogo
otdeleniya AN SSSR~-

vgjw~fllgf; PIRR"WWRT19
KISLITSD(,,.A.U.; TISHCHMO., D.V.; ADELO.. 148.; UUMST11p O.S.
Drilling fluid viscosity r9ducers froti wxO tar pitch, IsT, so
ucheb. haft' i gaz 3-noogt2l-26 %3, (MIRA hPU
--l. -lasotekhniaheskaya akademiya- i--Msesoyaznyy -naILqhno-isaledavatell dkiy-
institut burovoy tekhniki.
(Oil well'drilling fluldo) MaCQNity.)

TISHCHENIOt D.V.1 KISLI SYNp A.N.j_,ZAGAI*MTRj,_,,Q.j�,j PrinlmaU uehaatlyet
VAMHEVAr I.M*,, mlzdshI3r-u=chnyy sotrudidk; MITEYAIWVA,p L.Kh.;
SEMMVAI A.A*-#- *iadtho hnI7 sotrudizA - -
acids of -wood - tar -pitch -as .-raw- material. for
obtalning v1scosity- reducers. Sbor.trad.A"SMILM-4*o..141,',6-52 161.
(KIRA ~ 16:4)
1. Starshiv tekhnik laboratorli dreveany1di TEentrallnogo
nauchn6-issledovatellskogo I. proyektnogo inst tuts.'lesokriimichaskoy
proaVshlennosti. (for Mtryakova). 2 0 Vaesoyusny), nauch2o-
issledovateliekly institut burovoy tekhnikl (for S6menovi).
(Wood tar) (Phenols)
(Chemical tests and reagents)

MUCH, X.P.,doktor khtm.nauk; I.B.,kand.takhrionauk;
rA,URHI�m O.s.pimho
Nev viscosity reducers for c1rilling muds. Trtdy VNEIRT 9LO.I*.
142-156 '58- (MLM 11: 12)
(Clay) (Viscosity)

CIA
U~ A-ki, alpf ZaL -11
Sk-r. 34, NO- -1, 0" tXts
't, iInj -ot".fw4 --W~-. U44 ta Vvvrf Olt vj~--40~4itjLf tRLkhUl$
I itm! i - "ir fare, 4_4 phmej
'And arLill-'ok 5.cvcs4j tviv
by CFI,7.r,ur-;, Ertip, _ct. 2r,,t sirtml W~f-~ Vil-4
Oun. Lcir'Itite
w,cre aLa k-und rflvcti~r, xi ciulaiva
i 411Y in Ole ;;T cf~t!~T W. At, i-

ZAOARMISTR, O.S.; BALAYAN, L.T.
--mmmommo
Yield tests of the OFLN sulfurIced phenol as a viscosity reducer
of heavy drilling fluids. Azerb.neft.khoz. 35 n0.5:18-20 NY '56.
(Pmn 9.0 10)
(Oil well drilling fluids) (Phenols)

SHORYGINA, N.N.; IZUNRUDOVAP T.Vo; ADELIP I.B.; ZAGAM4I$TR# O.S.;
SALOHATINAs Z.T.
Prospects-for-the use of-bydrolytic lignin-in the protraloun
industry* Gidrolize i loookhim. prom. W no. 1:5-6 161.
(HMA 14 s 1)
(Lignin) (Petroleun industry)

A: I VM_xMTT_. I a, I flea &= RAW-t,
ACC NR. AP6012155 SOURCE COnE:' UR/04131166/000/007/0072/00
INVENTOR: Festenshteyn, M. S.; Krysin, Yu. P.; Zagarov, V. V.
ORG: none
TITLE: Device for testing samples of materials for thermal shock. Class 42,
No. 180388 10
SOURCE: Izobreteniya, promyshlennyye obraztsy, tovarnyye znaki, no, 7, 1966,
72-73
TOPIC TAGS: thermal fatigue, fatigue- test, combustion chamber, material testing
ABSTRACT: An Author Certificate has been issued describing a device for testing
samples of materials for thermdl shock in ZA~! jlow!'~ The device-contains a combus-
tion chamber with a programming element for controlling the supply of fuel to the
combustion chamber. To determine the resistivity of samples to thermal fatigue due
to thermal overload alternating with time, the actuating, mechanism ofthe program-
ming element is designed in the shape of a slide valve arrangement with a camshaft-
type electromechanical gear (see Fig. 1). Orig. art. has: 1 figure. [Translation)
[NTJ
1/2
UDC: 620.178.38-529

MW
L 42985-66
I ACC NRs AP6012155
Fig. 1. Device for testir4y samptIes 0fI
L
rrfaterlials. foil thekinal shodk.
1-Combustion chamber;
2-blow-through mechanism;
3- slide vabre arrangement;
4- camshaft gear; 5- time
relay; 6- power-supply unit.
SUB CODE: 131 SUBM DATE: 03Jul64/
r-f2rci 2/2 Iric

67CII'Vi, M.M.; KRYLOV) O.S.; SITUMp V.; ZAGA RUIA, SIA.
Effect of the composition and structure of vitrous slagB in
the -system -CaC --.; S102 - FeC - 11 0 and their- binding prcTert-lea.
Izv. AN SSSR. Neorg. mat. 1 no.2:3039-2;~3 N 165. (Mmk 18:121)
1. Laningradskiy tekhnologicheskiy Instititt imeni. Lensmrota,
Submitted May 10, 1965.

Vi Rini
vady SM41m9r;
Ito
."Ov.lvg jo sv*v..v J.4-A *1 'r Ito *Pcfi 'P InQ '"JJM'nP,1
Wa%-In !..Iljs) aalpvtoaamt
4
ILI
;tz. 1. limit "Ims,
;u1- -.9aa.16 012918 1
.01%b0ij Wts is OVID* allsoft-le.:
19W.6 v Wqg alulti. FT -vous-Im
k it I 'it: "at~ SIT..
pt" 1.2.01a it 41*0 SUI-19.4 qo1q. amemd, onsombe,
a 0 .*TV* T-VI20
:411 a*** "t, 0 "1
I *ft-16 a
9 Tole. Visa gimmits somae,
'!I' a -1.4, at David .92 vita Vaor%=* 0-3*7 snomommo
4714011 0-1 is -1110 is ... .Is a galolo., W074. *610%4~ somostpi";!-;~
-43 0 Rif) -8-* ml, 041 W1 01wfto vq3 WOJ4 we
No #"..be -a sea OlITS A 1 6*01
ON 4 1:8 217%.Sau 041 is 114,71Z.4
jo V.81.10 014% r~j VaDvidoll, 11 INN** 10 A.'a,
lsmlv D"Id
W:lj*~ worse Iowa WX -.9vqd ar,am.be *W3 sivi (a
1"911011 Only,
..%I -jo .... 0 ...1.4 Rd %STU I 411A al"as -00104 vr-96C
-J0j:q%.:2vl ..ad ljolow -view.) *,It& 54 Insup
:19 W 3goorliodw. me% Xq Glen&* 'm-lvus4ftW
is .'. 01 1 No
%
j vi :qq% !:.8v .6. - welt.r.. .11.6. a* ONIN,
TO u"121TIMb z %I: mv"vbv oql VON clu-940 041 *tomvmDp,;!
-1-1 VON lie 0401pul 0142 -.003`42% pit. att"411, 30 41OW
-owj ali.*J. .41 1 .01SION PaTV804"asou *RS *%*asp k
via
I I:ja-q% jrq I OvqeoAft*. C/t vivo
04 990 AbIli.o, v ... lie.* to ,.lc a'. Tlaw &Avtq
oil sera 30 U-12vagoloji 443 4,03 acems
so. % 4%;- va-low ohl to"I'l O= o"N"
100 to A'14.daid IwM to" a" OVID. or%VqglTv -P. ir IftV04
.'v.At.v It -Daox "qj (4 Vag 1(odude) '"Ximm
.111M.W ourind"JiOD 043 30 *111 at tied 04" ~Mmft
$U*I 40v~i I R." I ITIJI " A A.oU 'P." siou covZo, U*4XIO oIsomr.'I'i
VIP. ( NITS RVI.T at somdTio, saiwz~ Iwe -amda"t vivi a 0,
0. *Vqd vvi,m%tv am ul
Vqd vivivie I- v ...Wvzj Smoie"10 WIIAWW'
-1-1-6 *.owl ;1 9011vulds. ;b V.qz" ..11o"poid &a- v
U-66304 wals.-4 .00"ZID 1.0 Q%I. "120ammas, us vallsviste,
dd It 49 ZZI 70A *W"t *16,;Ss Imam TTleopwo
0T-%Xvi;oN* l*OuOv'q. -*Visa -avrolas, oij~' $210
a .. Zt:JO.
40MI-S om; A at-low so u4ji
4
.-T .1 -ab"USID-2 4-T
ddol -.4 -qN'oj --1 ."41" ..K . I
A,
C

ZAGARSKIIH, D.
Problems In the orgolgation of wMes In the food 1ndustryo Satme
trulsoool,109-63 N 056- 1011)
(Food Indus try--Pr:auc t ion standards)

Cand Mod Sci -- (dins)
zAGA*,JSKIIVfs M.G., !Irlieatzment of Resistant Stenosis of' the LA-
A
it
rynx with Preserved Tubes from, fleteregenous peritonom."
Uan SSRI, Kishi-
Ki-shinev, - 1957, 12 pp (Min of j1dalth iWMoldav
nov State Mod Inst), 200 copi0s (KL, 49-57, 115)
- 65 -

_ZAQKW&UJIy-)4wG.; SHOYMR~ A,p red.; SHEIMER's D., tekhne rrdo
I -aca4 -burns and-stenosis-of the-eeophigus; an- -
Treatment of te
experimental clinical study)Lechenie ostrykh ozhogwr-i steno-
zov pishchovoda; cksperimentallno-klinicheskoe isslodovanie.
Kishinev, Gos.izd-vo nKartia moldovenlaske,," 1961. 207 Pi
(MLL4 15:9
(ESOPHAGUS-440MIDS AND INJURIES)

------New method-of treatwmt-of-bmrnm-and Sears - Of--esophageea- gitenosis.
Trudy Kish.goo.med.inst* 13:n-15 160* (MMA 16:2)
14 lafedra bolezney ukhal, gorla i nosa Kishinevskogo goor-darsto-
Venno toinakogr, instituta*
ABD NALM) (MOPHAGU&-WOUM AND IN.TDMS)

UGMKMp H.G.1 YUZEMICH# F.S.
wW excretion-of gntibiotloo--by--poritonul-tulna.--Zdm-----
vookhranoWs no,6i42-" R-D 160, (MIFAIN12)
1. Is- bol I nitsy lechsa=prs~laniya (naolml I nik - Icud.med..'nauk M. G.
-Zagarskikdi) Hiaisterstva zdravookhrananiya MSSR.
(PLIO.ITONEUM-TWISPIANTATION) (ANTI:310TICS)

SOV/13i'-58-7-14074
_-Tratislation frorri., Referativnyy zhurnal, Metallurgiya,- 1958, 1'11;r1', p 13(USSR)
AUTHOR: Zagarskiy, V. S.
TITLE: Treatment of Products of Separation of Copper-nickel Matte
(Pere rabotka -produktov ot razdeleniya medno-nikelevogo
faynshteyna)
PERIODICAL: - Mate rialy- Soveshchaniya po vopr. intensifik. i us,oversh.
dobychi i tekhnol. pererabotki medno-nikelevykh i nikclt!vykh
rud. 1956 g. Moscow, Profizdat, 1957, pp 242-252
ABSTRACT:- - -The following conclusions are drawn from -1951-1953 studie.-I
at the Norill sk Combineon the roasting of Ni concentrate. Tbe
roasting of -Ni concentrate in multiple-hearth furnaces is more-
difficult than roasting of ground nickel bottom. The best results
are obtained in two-stage roasting. Investigations in sintering
r6as'ting e - ...-R-oastingin t~_e's_interin:g rpachin-e-
wer -carried out.
proceeds under favorable conditions: low -,;aicuum, high outgoing
gis iemperature, high output. To aVoid fc4sicn of thL-tsulfides,
the pr2cess must be conducted so that