SCIENTIFIC ABSTRACT GALLAI, T. - GALLAY, YA. S.

• Document Type: CREST
• Collection: Scientific Abstracts
• Document Number (FOIA) /ESDN (CREST): CIA-RDP86-00513R000614120011-5
• Release Decision: RIF
• Original Classification: S
• Document Page Count: 100
• Document Creation Date: November 2, 2016
• Document Release Date: July 19, 2001
• Sequence Number: 11
• Publication Date: December 31, 1967
• Content Type: SCIENTIFIC ABSTRACT

GALLAI, Tibor. ,
Critical graphs. Pt. 2. Mat kut kozl MTA 8 series A no. 3:
373-395 163064).
1. Editorial board member,"A Magyar Tudomanyos Akademia Matematikal
Kutato Intezetenek Kozlemenyei.11

GALLAI, Tibor
Elemantary correlations relating to the membare and
dissociative roints of graphis. Mat kut kczI MT~.. co
Seriss A no.lZ2:235-230' 14.
1. Editorial Board Member, ?'jV Magyar Tudomanyos Ak,-demia
Matematikai Kutato Intezetanok Kozlemenysi."

HARA ZT1, letvan, dr.,-. G"I. Zoltan, dr.
Role ofpenibillin In prevention of congenital syphilis. Dorgvogy.
vener. esewle 8 no.4:127-129 July 54
(S M ILIS, prevention and control)
prev. of congen. syphille 'by penicillin)
(MICILLIM.'ther. us~
syp&l1s. Cowen.. prey.)

Z- q1
RACZ, Istvan, dr.; GALLAI, Zoltan, dr.; IULDRS, Miklos, dr.
Data on action mechanism of unsaturated fatty acids in the
therapy of childhood eczemas. Borgyogy. vener. szomle 9 no.
6:225-228 Nov 55.
(LIBDLEIC ACID, therapeutic use
eczema with hypochromic anemia in child, with linolenic
acid, eff. on hematopoesis.)
(FATTT ACIDS, therapeutic use
linolonic acid with linoleic acid. in eczema with
by-pochromic anemia in child. eff. on henatopoesis)
(ECZENTA, in infant and child
compl.. bypocbromic anemia, tbar., linoleic
linolenic acid, @ff. on hematopoeais)
(ANWIA HYPOCHROMIC, In infant & child
compl.. eczema, ther.. linoloic & linolanic acid, off.
on hematopoesis)

RACZ, Istvan, dr.; GALLAI, Zoltan, dr.
Chlorpromazine in the therapy of skin diseases. Orv. hetil.
97 no-15:398-399 8 Apr 56.
1. A Nephadsereg Ignessegug7i Szolgalatnak koslamenye.
(PSORIASIS, ther.
chlorpromazlne. results. (Hun))
(BUFMA, ther.
'lame)
(BLISTIM
form., exper., Induced by lodoacetic acid. off. of
chlorpromazine. (Hun))
(CEWRPRDMAZINr-, tber. use
eczema, psoriasis & exper. blister form.. results.
(Hun))

EXCERPTA !%LDTC.I~ Vol., 11/7 ju-c -7
13
1815. IIACZ St. and GALLAI Z. Budapest. *Angaben zur Rolle des Lar'.f--Ctil:; bei
der Behandlun~ einiger utkranWiciten. The role played by 1.7r-ac-
til in the treatment of some skin diseases DERM.VISCIER.
1956, 134/28 (7.70-773) Tables 3
Largactil, 3-chloro-10-(3-dimethylamijiopropyl)phenothiazine hydrochloride,
inhibits the function of the parasympathetic, lowers the blood pressure, is --nti-
spasmodic, sedative, antipyretic and antihistaminic. Six patients with psoriasis
vulgaris, and 16 with various types of eezemas Were treated with largactil, 3
doses of 25 mg. There was no visible effect upon the cases of psoriasis but in
the eczematous patient3, a marked reduction or complete disappearance of itching
and thus improvement of the pathological picture. was observed. Rust - Berlin

USSR/Chemisir~ ... ;00_ 'Oxygen~ Chlorine Production Aug 5~
"Method f or Separate Catal:~tic. Production of Oxyg*n
and Chlorine From Ca(CIO)2, It V.'M. Gallak
"Zbur Prik Xhim" Vol XXIV, No 8, PP 798-8o6
C&(CIO)2 with small amts of catalysts at low timps
can activate oxidation pr~ocesses, while Oj-mll'y be
p-.epd with larger amts of catalysts at-higher temps,
Catalysts are oxides of Ni, Co, Fe, Cu, Md,., most.
"tisfactory for development of 02 being Co+Fe in.
3:2 ratio. Gatalysts and C&(ClO)2 will not int64Mct
it absence of H20. Inexpensive, available Ca(CI6)2
l9m26
USSR/Chemistry - Oxygen, Chlorine* Production Aug 51
(Coutd)
c= be used to replace very scarce KC103 (for produle
ti6n of 02) and compds or Ym and HC1 (for prodiicti6n'.
of C12)-
'19=6:

OALLAK, V.M.;,,DELINSKAYA, N.I.; PAVLOVA, T.A.
Ghlorination of methane by chlorine oxide. Zbur.prlkl.khim. 38
no.11-2599-2602 N 165.
(MMA 18-~,12)
1. Submitted October 14, 1963.

G;, I ', 4 K V 'I' E3,-, INSKAYA 11. L , T, t,
) -1 11 * y , - , ,
Method of pr-aparing chicrine .~xjde,, --P rG.6,1.22~7
1229 j~~ 165. (K1 11 '! 81 110')

GALIAIII A. inz.
Final reports on scientific research tasks assigned by the
CzechoslovaOk Academy of Sciences, aAlding and Architecture
Institate of the Slovak Ac.-W:my of Sciences, Bratislava.
Stdv Cas 11 -,C'.8.-A3 163.

I r7AI',.'ESCU,7.; NEGOW: ,
MEGHEA C.; DACU, Gh.; CONISTANTMESCU.M.; S U Y4
Our wxporitvico with the one-stage complex surgical cure of
complicated thoracic tuberculous spndylitis. Rumanian med.
rev. 7 no.3-- 70-73 Ta-Vx'64-
4-

CALUSINSKI, Bogdan, mgr.; GALLAR, Jan, mgr. inz.; SKORUFA, Andrzej,
mgr. inz.
Testing pressure welds in steel constructions with the ZSX-2
magnetic flaw detector. Praegl. spaw 15 no.10:228-229 0163
1. Akadenda G)rniezo-Ilutnicza, Krakow.

GOLECKI, Jozef; GALLAR, Jan
Design solutions'and computing methods of blast furnace skip
hoists. Probleny proj hut maszyn 1-2 no.W29-236 Ag 164.
1. School of Mining and Metallurgy, Krakow.

I
CALUSHISKI, Boadan, mgr.; GALLAR, Jan, mgr. inz.; SKOIRUTF.., Ind-mej, MEr. Lnz.
~, ;netic method of tooting butt welds. Przogl opaw 16 no.7/8,.
189-190 il-Ag'64
1. Technical University9 Czestochowa (for Calusinski). 2. School
of Mining and Illetallurgy~ Krakow (for Gallar and Skorupa).

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-ASSOCIATION.:, Poutec km zest_066~~k~ stooho~4n
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Gall~iA, Akndeni1I4
Gorn1czo;4Iot1d za;qri
(Goleckf
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TOMANEK, A.; PULPYTEL, Jj_GALLAS, J.
A new method of measurement of respiratory movements of the bronchi.
Cesk.otolar.9 no-5:271-273 w6o.
1. Vyzkwmy uetav tuberkulozy v Praze 8, re&itel doc.dr. R.Krivin)m.
(BRONCHI physiol)
(RESPIRATION)

ACCESSICIff NRt AP4033066 P/0034/64/ODD/004/0168/0269
AUMORt Calusinak49 Dogdan(T64dusintaki, B.)(Mater in artsh Gallar. Jan
(Maoter engineer)
TITM: The translator magnetic ZSK-l flav detector -
SOME: Fomiaryq automatyka, kontrola, no. 4, 19649 168-169
TOPIC TM. flaw detector,, bridge detector, ma tic rim detector, ZSK-~
f law detector
AWTMCT.9 The authors desigaed the ZSK-1 because of a lack of this type of Vuxw
detector In Poland. -The design is based an detection by the bridge method. The
Instrument (Fig. 1) consists of an HC traneistor generator vith acoustic frequen-
cy, a bridge measuring system,, a transistor amplIfier,, and receivers. It has & .I
frequency f - 1000 Hz,, an amplitude of electric motor power output E0 = 2 V, a;A
an output Impedance RoUtMt, n X kAe It detects flaws that am 1 = in diameter,,
located at depthe of 113 nzim* A slight change in the shape or d4men ions of the
core in the measuring s7stem makes the Instrument suitable for detecting 'flows
due to diminution, Inclusion,, and co6centration of strain In ferrazagnetic
matex,ialo,, for studying the t4dakaeas cC ferromapetic plstsa,, sad for studying:,
rcr

ACCESSI(IN XR: AP4033066
the thicImess of fall or coatings made of nommetallic materialeo Work to Im-
]prove the. ZSK-l f1m detector continuees Orige wto hu: 3 f1gurese
ASSOCIATICKs Politieftnika Czestochowsks- (Cmetachaim Mytedbuic): AkadaWA
01
77
000-

H, -I WINI U-111141 r~PqOrgfl~ F,17 I Fit I IIIIIN,
ACCZSSION.NRI AP4033066 INCLOGUILE: 01
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of the
Fig. Ii schawaic aiawma
ZsK_I flor aete"Or
fteosUft; .2 PIp ad P3 - PO-
t=Uawtenj 3 W ghdt4b.

SABACKY, Vladimir, inzz.; HOMIOLA, Bedrich, inz.; VAVRA, Miroslav, inz.;
GALLAS, Jan
Effectiveness of the construction of main lumberyards depends
on the use of heavy duty machines. Les cas 11 no.3:249-272
Mr 165.
1. Enterprise Management of State Forests, Brno (for Sabacky
and Homola). 2. Forest Enterprise Tele (for Vavra). 3. Forest
Enterprise Rajnochovice (for Gallas). Submitted November 3,
1964.

C A
plommift WA696 twumvIton ift ON so am . Wo-
Wo.
ziffoi-ill It-sver mills 1% fflqnvk~l
thr view me ighfillfrial Petmonvy stream jvftill~vot, mrs.1
fir"wvvy o1 fihrr moul other vow mmvr~~%. V4111,11. 11WIt".1,
of while-water trwalinerst twkw It, 0% rrinsw inti, %Irrm"i%,
"'Ch putirubf rm p&--' V-1k. arr J-
rribpd r. R ZeCTIV

Ij
GA LLLS P't.
"The Massey Coating Equipment" p. 26. (Przeglad Papiernic , Vol. 9, no. 1., Jan. 1953, Lodz)
SO: Monthly List of East European Accessions., Vol. 3., No. 2. Library of Congress., Feb. 1954

v`V
GALLAS, W.; RZYSKT, J.
How operational difficulties of papermaking macbine No. 5 were overcome in the
Paper Factory of Myszkow. p. 237. (PRZEGLAD PAPIERNICZY, Vol. 10, No. 8, Aug.
1954, Lodz, Poland)
SO: Monthly List of Eqst European Accessions, (EEAL), LC, Vol. 3, No. 12, Dec.
1954, Uncl.

GALUSI ~'.
GALIAS, IV. Modernization of the paper machine, to impro-ve pruiucti.cm. '1. 2710
Vol. 12, no. 9, Sept 1956
PRZEGIAD PAPIEMICZY
ISCHNIOLMY
Lodz, Poland
So., East European Accession Vol. 6, no. 2, 1~57

GAI LA3,
Modomization of the ci,,,-arette-paper rr,;chine
P. 45 (PPZELGAD PAPIE%.ICZY) (Lodz, Poland) Vol. 13, no. 2,
Feb. 1957
SO- Monthly Index of East European Accession (33SAV. LC Vol. 7, No. 5, 1958

- GALaS, Wojciecb) inze
Automatic paper sorting. Przef,,l papior 1~i no.l~: 383-3806 D163.
1. Biuro Projektow Przomyslu Papierniezegop Lodz.

GALLAS, Wojciech, inz.
Radiclon type hydrocyclone cleaner. Przegl papier 20
no. 1: 18-20 Ja 164.

(" - f L- ~.-, , 1; 0, i (. i J, i; , i F -,
4 .- -1 1 - I
A 1, ri 1 i -!~ i, 4
~ on cf pneumatl !n -1,r- wv: p-p--r
j..1duz-tvy. Pt.. ',. llrzogl partar 20 no.6:1.83-.-,J~6 . ,e. , c,,,. .
I . Dmsign Off of Oin ilayor lrl,i~;.ii. r-yp I

GALLAS, Woiciech, inz,
Use of pneumatic transportation in the pulp and paper industry.
Pt. 2. Przagl papier 20 no.7:218-222 JI 164
v
1. Design Office of Paper Industry, Lodz.

STASINSKT
"9 Witold, mgr inz., GALLf"15, Wo'ciech, 4r?,.
-1 ..". -- - ~;~~ .-
Paper machine flo-4 in the Szczecin Pulp and Paper V,11II. r
Skolwin. Przegl papier 20 no.10?1123-329 0 f64.
1. Szczecin Pulp -md Paper Kill, Skolwin (for Stasjnflk.~~..
2. Design Office of" Paper Industry, Lodz (for GnIlRs'.

-~x orienc,,s. 01.

9; V
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TRET'YAKOV, Aadroy Vladimirovich- GALIAY B.M. redaktor; VALOVI N.A.,
0 W ~~ &
redaktor izdatel'stva; KiMW~~ekhnicheakiy redaktor
[Rolling thin strips] Frokatka tonchaishet lenty. Koskva. Gog.
nauchno-takhn.lzd-vo lit-ry po chernoi. I tevetnoi metallurgii
1957. 96 p. (KIRA 10:71
(Rolling (Ibtalwork))

GALLAY, Michalp inz.
Waterwork of Velka Domama. Vodni hoop 13 no.1:37-38 163.

_,42f"9
., e-
S 1') 0,116 2/0G'0./0034,1 C 0 1 /00
/91 L1100 D2-1-9/D-1401
AUTHORS.- Kibardin, Yu., Candidate of Technical Sciences~ and
l ~a ~Honored Test-Pilot of -the USSR, Hero of
Gal
TFe___Soviet Union
TITLE: Barrier of the unknown. Engineers look forward
PERIODICAL: Znaniye - sila~ no. 3, 19629 17 - 19
TEXT.- The article is based on an incideni in a Soviet feature film
"Barrier of the Unknown". which is shortly to be released. A super-
fast test plane (no undercarriage) is cruising at 5,200 km/hr at a
height of 929000 meters waiting to be picked up by the carrier pla-
ne, A blue glow suddenly develops outside the plane and envelops
the whole fuselage. However, it is not sensed by the pilot and is
not recorded on any of the instruments. This phenomenon is then
left to the two authors mentioned above to explain. Kibardin gives
two possible explanations of the phenomenon. 1) The temperature of
the boundary layer rises sufficiently to cause molecular dissccia-.
tion of the air and the formation of atomic oxygen and nitrogen.
Card 0

S10041621000100310011001
Barrier of the unknown. Engineers D298/D301
These then --ater into chemical reaction to form nitrous oxide, a
gas that can glow at high temperatures. Although the Slow is of no
dangerv the active atomic oxygen may enter into reactions with the
superheated metal fuselage of the plane, weaken its strength and
lead to an explosion. 2) Through friction with the air the plane
may become charged to a very high potential and become a source of
electrical discharge in the form of a cold glow. Gallay gives no
explanation of the glow phenomenon but describes the'development up/
to the end of World War II of the launching and recovery of planes
from a carrier plane in the Soviet Union, Persons mentioned as con-
nected with this development are: Aviation Engineer V.S. Vakhmis-
trov, Test-Pilots Anisimov and V.P. Chkalov,, Pilot A,,I,, Zalevskly,
Test-Pilot V.A,, Stepachenok, Captain Arseniy Shubikov The autbors
point out that nobody has yet seen such a glow as is described.
There are 6 photos.
Card 2/2

L 201,49-63 ;t

special Aircraft
Features in Piloting Jet,
Ch, IV, Range and.Duration of-F4ght
Ch. V. Pilot Spin,and Re
ins OOVGX7

ph* vx*~, Oft
Landing Approach and Touchd

Cho, VII. SpeolaPPeaturee on the Control of the Rmdderklf
Aileron.. and Propulsion Systems,. of Jot'Airowt, 179-'
Automatle electronic deirIces for simplifying con-

trols, already in use, plied'on a Ili
will be ap
scale, as will cybernetic piloting units The
-fuel devices used on all moderns jet *,an
automatic:
~ _gines'independently regulate the engine to the
flight program designated by the pilot with a,
weingle jorliF of the control lovera*.

Library of Congress
SUBJECT t Aerospace
FC_/I

t
d
AD/Ak/

0
3 /6
7
iF
3/3
'I MIN .
/

~mm#' M. 1.
Opredelenie profilinogo soprotivleniia la-jla samoleta v polete retodom
impullsov. Moskva, 1938. 36 D., illus., tables, diarrB. (TSAGI.
Tekh--iicheskie zanetki, no. 161)
Bibliography: D. 36.
Title tr.: Determination of profile drag in flight by momenttur. measurements.
Ell
TI,170.146 no. 161
SO: Aeronautical Sciences and Aviation inthe Soviet Union, Libracry of
Congress, 1955.

GAWAY, M.L.
V111anis skarostuop polls vokrug mmleta na pokazanila alltimetrov i
barografoy. (TSAGI,, Trudy, 1939, p. 3-9, illus., diagra.)
Title tr.: Effect of velocity distribution of air around the air-craft upon
indicators of altimeters and barowters.
Qk91l.M65 no. 427
SO: Aeronautical Sciences and Aviation in the Soviet Union, Llbraz7 of
Congress, 1955

L L
GAL14 M.L.- and B.N. EGOROV.
I
Ismerenis tem~eratury narushnogo vosdukha Y polete. (TSAGI. Trudy, 1939, no. 427
p9 6-8. diagree)
Title tr.: YAwsurements of outside air temperature in flight.
QA9II.N65 no. 427
SO: Aeronautical Sciences and Aviation in the Soviet Union, Library of
Congre3s, 1955

Go Lduchshenii ixodollnoi usLoicnivosti seriinykri sa,.-uletov. ('re'-:."L:Iika
v:-zdushno1:o .'Llota, 19h5, no. h, p. 1-7, 17, diaErs., ;ALI-iofraphy)
Title tr. : Improvement of longitudinal stai)ilit~ of iirplane.,; pro~--ucec
in neries.
T1,504J4 1945
SO. Ac-romAical Science and Avi.,ition in the. Soviet Union. Library of
Conp,ress, 1,,55.

GA,,~Lzle_,V
AUTHOR:
17" Z,
86-5-5/24
L., Col, Test Pilot, First Clasa, He-x%-~ c-tf Vie
Soviet URIF-c-in, Candidate of Technical Scienaee
~;ITLE: Takeoff and Landing of an A.Lroraft with a Bi!:--ycle Land'_' 1-4g
Gear (Vzlet i posadka samoleta a velosipednym ahasai)
PERIODICAL: Vestnlk Vozdua1xnogo Flota, 1957, Nr 5, pp. 27-34 (USSR)
ABSTRACT: A bicycle landing gear (Figure 1) consists *f the twr;
main stmts, idiieh are located under the fuselage, _'n the
plane of the xtraraft symmetry, and of two wing 3"'.ra-t-a.
The weight of the aircraft Is usually distrilyated alm. ~, at
equally batween the main st*nits. The wing atr,,ata mr-,
used to prevent the aircraft- frmn banking when r2(. vea
on the groland. They carry only a very at'nall part of -t-ha
aircraft's welpght. A bicycle landing gear has no lls~adency
toward directional inetability and spontanao-L,3 tuvns while
-moving on the ground. It has perfect visibility while;
taxiing. Its piloting is somewhat dirrerent. Thq oentrol
and the braking actions in an aircraft eqwLpped-Vith a
bicycle gear are independent of one anot]7,.er. It
follows that the braking may be of any strength, that a
nonsynchronous adjustment of brakes or getting a wheel
onto a slippery or wet section of the landing strip V-_~fect
the direction of motion or the braki4ng reg:Lme of tthe air-
Card 1/4 craft. In addition, a rot--ating frcrt strnt permll-ta

86-5-5/24
Takeoff and Landing of an Aircraft with a Bicycle Landing Gear (Cont.)
settltng and maintaining the required radiLm of turn
more precisely and makes easy the directional control
of the aircraft at a side wind during takeoff on a
landing run. An automatic increase of the attack angle
during the takeoff run by means of the "squaV' of the
rear strut or the straightening of the front strut
shortens the takeoff run distance and makes the takeoff
independent of the action of -the pilot. There is a
diagram (Figure 2) showing the variation of 'the attack
angle during the takeoff run of aircraft with a bicycle
landing gear and an automatic increase for the takeoff.
Attention should be directed to the fact that the attack
angle of an aircraft with a bicycle landing gear cannot be
controlled during the takeoff run up to the moment of take-
off and depends only on the design parameters of the air-
craft. Aircraft of small and medium tonnage are sometimes
equipped with a sem"L.-bicycle landing gear. It is like a
Card 2/4 three-wheel landing gear whose nose wheel is left anchanged,

86 - 5 - 5,/2 4
Takeoff and Landing of an AirorAft With 5 Bicycle Land~uig Glear /Cor_'t.
while the win wheels ara sqlaeezed tDgpther and can be
withdrawn Into the fuselage as one carriage. The main
wheels of these aircraft are displaced tc the rear from the
center-of-gravity farther than in the classi,,- three-wheel
landing system. The takeeff of an aircraft with a semi-
bicycle '-landing gear differs from that of an aircraft with
a bicycle landing gear, The former takes off J-n an cndinary
way by lifthig the nose wheel and creating a fore-and-aft
angle durLng the takeoff run. There Is a schematic drawing
(Figure 3) showing the basile moments aotljig upan the air-
craft in a longitudLnal plane when the ai",rer-aft is moving
on the ground wIth a lifted rose wheel. 111 is evident that
the moments are created by a rxeight; forse, G, a 11ft force,
Y, an aerodynamical resistance force, X, a 1:fft force of
the horizontal empennage, Yr.0, and a thrust for-'e of the
power plant, P. Whan the aircraft moves on the gro-und,in
a side wind,, there always appears the 1-345'eral a erodyr-a mica 1
force Z r b N1 - N2) (Figure 4) strivLng to overturn the
Card 3/4 a1rcraft to

86-5-5/24
Takeoff and Landing of an Aircraft with a Bicycle Landing Gear (Cont.)
an-uneven distribution of the load on the left and right
wheels of the landing gear (h is the distance between the
po=' of application of the force and the ground, b is
half of the track gauge of the landing gear, and NI and
N are the forces of the earth's reaction applied Eo the
w9eels). The reaction force of the earth appearing when
the front landing strot touches the ground creates a
moment about the center-of-gravity of the aircraft which
favors the increase of the angle of attack. As a result,
the lift force increases and the aircraft repeatedly
leaves the ground. Such bouncing may become progressive.
The pilot of an aircraft with a bicycle landing gear twabt
pay special attention to make the landing on the rear strut
or on both struts simq1taneOusly. There is a schematic
drawing (Figure 5) showing the position of the bicycle land-
ing gear with resp6et to the earth's surface during the
takeoff and landing. There are 5 figures.
AVAIIABLE: Library of Congress
Card.4/4

sov/86-58-10-23/40
AUTHOR: GallV M L., Col, Test Pilot First Class, Candidate
-6r-N6 '~Nfj471 Sciences, Hero of the Soviet Union
TITLE: Lateral and Directional Stability of Aircraft (Pope-
rechnaya i putevaya ustoychivost' samoleta)
PERIODICAL: Vestnik vozdushnogo flota, 1958, Nr 10, pp 49-53
(USSR)
ABSTRACT: A discussion and explanation of some stability phenom-
ena, especially of those which, the author states, are
often misunderstood. AS Boon as the aircraft changes
its direction of flight by the action of turbulent air,
the aerodynamic banking and yawing moments develop im-
mediately. The yaw is righted by the directional
stability. When flying in bumpy air, the overwhelming
majority of bank attitudes are not caused directly by
the turbulent air but are reactions to divergent mo-
tions. The lateral static stability is manifested by
Card 1/4

Lateral and Directional Stability (Cont.) sov/86-58-10-23/40
the appearance of a lateral moment which banks the air-
craft in the direction contrary to the divergent mo-
tion. The lateral and directional stabilities are the
main factors which affect the character of the lateral
movement of the aircraft; the designer can, by con-
trolling these stabilities, control the lateral move-
ment efficiently. However, by making the lateral
stability too effectiVe, the aircraft may lose its good
flying qualities: it would tend to bank excessively;
this phenomenon has been often mistakenly understood
as the manifestation of poor lateral stability. In
multi-engine aircraft, as soon as an.engine located on
the wing stops working, the aircraft starts yawing; it
continues flying byinertia in the same direction.
There have been aircraft with a much too excessive,
lateral stability, and therefore they tended to be un-
safe; they banked very heavily and even turned upside
down. To prevent this, not the ailerons but the rud-
der was used; it then removed the initial cause of
Card 2/4

Lateral and Directional Stability (Cont.) sov/86-58-10-23/4o
banking. In aircraft with a "neutral" lateral stabil-
ity, which is the desirable property in all aircraft,
there is practically no banking in such cases of engine
failure; the pilot then eliminates the yawing by ad-
justing the rudder trim tab. Excessive lateral
stability is especially dangerous with turboprop engine
aircraft because the propeller of a stopped engine'de-
velops a heavy drag (before its blades are feathered);
a sharp bank can develop even when, at a moment of a
raised thrust during power approach, the thrust fails
to rise synchronously in all the en&tnes of the air-
craft. An Increased directional stability Is quite
useful; it lowers, in a degree, the destabilizing ef-
fect of excessive lateral stability in cases where the
value of the lateral 5tability Itself cannot be low-
ered and also in the moments when the thrust fails to
be symmetric. A high directional stabillty simplifies
substantially the task of the pilot when he executes a
turn since deviation from the correct attitude of the
Card 3/4

Lateral and Directional Stability (Cont.) sov/86-58-10-23/40
aircraft develops immediately a strong righting yawing
moment. A high directional stability of the aircraft
makes piloting more effective and flying safer.
Card 4/4

GALLAYRI M., Geroy Sovetskogo So7=a, zaaluzhenny7 letchik-isp7tatel' SSSR
.1 ~j
Test pilots. On. tekh. 4 no.9:24-29 S '59.
(NIRA 12:12)
(Airplanes--Ylight testing)

,GALLAT,_N',L.-,--Geroy Soverskogo Soywa, zaslushenny-y latchikispytatell =R,
kand.tekhn.nauk
Flying with uncomplete and uneven thrust. Vest.Vozd.lPl. no-3:53-60
Mr 160. (MIRA 13:9)
(Airplanes-Aerodynamics)

GALIAY 14. ."
Beyond the sound barrier ("The lonely si~,- by William
Bridgeman and Jacqueline Hazard. Reviewed by, 14.Gallai). IUn.
tekh. 4 no.1:42-44 Ja 160. (MIU 136)
(Jet planes--Flight testing) (Bridgemn )William)
(Hazard)Jacqueline)
I\

GALLAY, M. Gbroy Sovetakogo Soyuza, zaaluzhennyy 1otvhJk-ispyt&teV SSSR.
American pilot Everest's book ("The fastest man alive" by Frank
K. E.verest).Reviewed by M. Gallal. Grazhd.av. IS no.1:11 Ja 161.
(MIRA 14:3)
(Airplanes-Flight testing)
(fteresti, Prank K.)

GALLAY, M.L.; VASILIYEV, A.A., red.; MIKHLINA, L.T.J. tekhn. red.
(Piloting jet airplane:]Osobennosti pilotirovanila reaktivnykh
samoletov. Moskva, Iz -vo DOSAAF, 1962. 195 p. (MIRA 16:2)
(Jet planes-Piloting)

.qAJtW,__Mnrk Lazarevich, Goroy SovotBkogo Soyuza, zaal . letcldk-
ispytatell SSSR; FEDGBRIKO, V., red.;" GRIGORIYEVA, Ye.,
tekhn. red.
[Through invisible barriers; from the notes of a test pilot]
Cherez nevidiWe barlery; iz zapisok letchika-ispytatelia.
2. izd. Moskva, Molodaia gvardiia, 1962. 124 p.
(MIRA 15-8)
(Airplanes---Flight testing)

'I IT! I I F!!! WPNiq lvimfAl!i~ ~Sju 11111i IF" p jg'
11-Va 4) E14T t 1), ~Aj 17C- MIT MIN; ASD~,Ukl~',)
-12
1 -6 EPR/kPA(b)
7: 14CCESSION NR: -AM3001368 S/WCQ/62/6~0/000/40OV6196:
AUTHORz - Gallay, M. Lo
wi
..TITLE: samol t 0 ecial f6atures
Osobennosti, pilotirovaniya reaktiv4*kh e 0v, n
loting:jet aircraft)
pi
etov,:;ibskv~p :Izd-~vo DDSMY'
SOURCE: Osobennosti pilotirovaniya reaktivrV*kh samol
196?1 Ill 12,,~ 15p: 92p 11158 190
TOPIC TAGS: aircraft control systemp boundar'y-layer'contiql os6illation dampar~
cybernetic piloting unit
ABSTRACT: The following points of special Interest are mentionedt:. 1) A number.
of designs for the control of a wing's boundary layer have teen,drawn up, and
the first.idMd-L~t id flight tests have given positiv ssults~ 2) a
&=eLl aj e r Th
spontaneous oscillation of an aircraft at:higk altitudes J.9~,blimiin~ted by an:
c1scination damper, which is part of the control syst6ma.-.- The da~piir automwLically
compensates for aircraft oscillation, and alichiev!sd with one
1motion of the controls. 3) The automatio.electronic devices for:sImplifyingf
controls already, in use win be applied on a. large scale# 6b will
iloti
1P pa 4!4t-s- 4) The automatic devices are used on an naderh:j~t engifies'to
LCard 1/2.

GALLAY, Mark Lazarevich, Geroy Sovetskogo Soyuza, Zasluzhennyy
-- . ';1e_t6hik-ispytateI1 SSSR; FEDCHENKO, V., red.j SAVELIYEVA, V.,
tekhn. red.
(Tested in the skyi continuation of the memoirs of a test
pilot, "Over invisible barriers."] Ispytano' v nebe; pro-
dolzhenie zapisok letchika-ispytatelia "Chere3 nevidimye
barlary." Moskva, Molodaia gvardiia, i963. 267 p.
(MIRA 16:10)
(Airplanes--Flight testing)

KOTIK, Mikhail Grigor 'yevi, h, kand. ttekhn. nauk;
Vasillyevi-ch, inzh.; PA3HKQV&,IY, I-or' Mfikhaylrsvi::~-,
kand. tekhn. nauk; SARDANOVSKI-f, Yuriy Sergeyevich, ir-zh.;
SHCHITAYEV, Nilcolay Grigrr'7evich., inzh.; G4LAY, IMI.L.,
kand. tekhn. nauk, zasl.lotahik-ispytatell SSS~*I, retgenzen-,;
KIRILLOV, Ye.A.. inzh.~ relLsenzent
(Flight testing of airplanes] Letnye ispytaniin smoletov.
Moskva, Mashinostroeniq., 3965. .3,,'9 p. (MRA 18:11)

GALLAY, Mark Lazarevich, Geroy 5ovet'i'l-0,170 '30,111za, Z"I:ij- letc-ilk-
FEDGIIENKQ, V., red.
[Through invisible barriers. Tested in tho sky; from the
noten of a test pilot] Cheraz nevidlmye barldj*y. T-%pytano
v nebe: Iz zapisok letchika-ispytatelia. Mcskva, Moloda�a
gvardiia, 196~. "5 P. (F-I!U -10-t)

ACC INR: Am,6004547
Monograph
UR/
Gallay,Mark Lazarevich
Throu8h invisible barriers. Tested in the sky, from the notes of a toot pilot
(Cherez nevidimyye barlyery. Ispytano v nobe; iz zapiaok lotchika-iapyta-
telya) Moscow, Izd-vo TSK VLSKM "Molodaya gvardiya", 65. 044 p.
100,000 copies printed.
TOPIC TAGS: pilot.training,, jet aircraft
PURPOSE = COVE-RAGE: This book is an account on tent pilots vhoso-.voee, if)
very important, for the perfection of aircraft. While writing about these
nen, the author tries to limtt the subject of aviation technology to a mini-
mum necessary fob the understanding of the work of a test pilot. Unfortuna-
tely, the author never kept a diary on his flights and was forced to rely on
his memory. His reports contain some factual inaccuracies.
TABLE OF CONTENTS (abridged):
From the author
Card 1/2

ACC NR: AY,6004547
The beginning of beginning -7
I become a test pilot -31
Flutter -56
First jets -86
Tested in the sky
Success and failure-127
TTU-4 far, high, fast (4162
Tests of TU-4 continue -199
About courage, risks, time and many other things -231
Yesterday it was exotic -268
Flying techniques and flying ethics -312
14ore about flying athics -349
Qne hundred twenty four -375
Rer-ords and record holders -411
Test pilots today -429
SUB CODE :04 OOUBM DATE: 29mar65
Card 2/2

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11 Is Ilui 1wroalin, or Jim lortal on ths- wilit iin Immil Iripot -Iin,i-l
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Imth with and without hilwitation and it 6 ithown thtt for a givol
Ml~$Vtiiill the UHlHfWr Of lUtM% Iluj.Y IN' n-411913-41 I)V hillf` i( Iljr VoMwt
lubricant is employed. Woo-ferrous metals were employed ror these
investigations.
40
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WWA !
0 0 oft
IIIII I Litz Bois 24P)IM jell I, I] I- it V mile -t 1113 mds.20
A'A f a 0 U+il- j I .-I I A I- It, 4-1.1.11-V
O'S'.4cWt ..a f.C.C.1q;
00
lee
CboWofLubti"nUWCo)A-RolHigotMOAAbSUdAllOM L.M.
l1avlov and I'll. N. UL1.6p.. (Kneliesivennayn '.still, 193S. No. 2,
-00
fil). 34-4:1). (111 ltli=? By may of introduction the litithorti
00 ISUH111111dw the functions of it lAricant durit%g roffilig and M.Vie.A i(s -00
00.t tiesirablepropertit-t. The laboratory investigation took I fie forin ul"a X60
Ole study (if a large number of lubricantet, the effect of their use during, =00
ridling oft the specific pretwure and the elongation of the material, '40
t lie effect of lubricants in different types (if rolling mil.1 and on the
006 Zoo
Wongistion. of different metal.4, the effect of additions of free fattv
OOV too
iscids ittid of vegetable oilis to the lubrimitts, the Imisgibility of usbu'x
00 is mixtures of machine oil and pitraffin oil, mrriliiion tmts in Varioll)l -09
lubricantit and, finalky, a study of the behavi-3tir and tho iffect of
S
IRA4
hibrivants during annealing. Stee h Carboll 0-091/0) was UM41
wineexileritnentm were altwo
in the tritlJority (if the experiments,
conductei I uyj braim, copper and slutni:niuni.
goo
lie*
011FALLUACKAL LITtRALTIM CLAWMATIOM 000
it sold#.) .41 C". ant .31,11 CW 0- 0
0 0 1 Ir a 1) .8 4.
U W to ,1; 10 At: 'T, K (C a "a A 1 14,
is 0 0 0 0 0 0 0 0 0 0 * 0 00 big
- -------- --

.~A
A
A
00
*0 a
*0
00
0 A
0*
004
00
0 0 0 0 0 0 0 *--Go**
.-tq- -.0 1"* FR Let
TICS -.01.
A-)- J-1
Madk D11MONdoi-id "Nse-MM Ulu 1. It. Pavlov and
The autV~6'revlew previous work on the bending of rolls awl
ConAider the various expreasions arrived at for the magnitude of
the elastic deformation. Three formulaam generally too involv(4
for practical use. For practical purposes the authors derive the
follwAing expression for the deflection of the rolls
nPP
3114 x Er X
where P is the prenure, E the modulus of elasticity of the material,
1 t tie effective length of the roll between the hearings, I the moment
of inertia of do rolls and a a coefficient depending on the ratio of
the width of the strip to the length I of the rolls. Using a special
apparatus. the measured deflection of the rolls was found to affm to
within 5-10% with the reaults calculated from the above fortouls.
The formula should be useful for calculation& in connection with the
cambe-ring of rolls.
6 1 a - I _!!TALLUN!!c~tL U191PATUM CLAIWKATOO
C."
SoNat) 411 ON;-Qit-
$111114. 011111 OK O"V III
"I* or trivir ix 8r& its Itit; it ;jO('W v114: i0s vow o.%:,%*w9a4 v V
t Its
Vo
-00
a*
SOO
too

0 so so* 0
4161 4 i~fil, - ,
1 8 IS 6 1 a I to If 11 il 1, .11 16 1, 111 to ?I X 11U%J109"MUMP Q 4W 1) 41 U4, r 0
A.4 C. -0- R-A I U.J.J., A. k 0 0
OOA 'At - "R-L"p- ~_,Pfrkl_
1,11"Itsill ko PovP1101.1% "N.
ea
:0
j yo So
ELASTIC CMPRESSION OF ROLLING-MILL POLLS. 1. 11- PSVIOV and
4r 1-00
Gajlayf~. (MeteillulL, 1938, no. 1. pps 79-86). (121 Russian).
Earlier literntu an the radial compression of' rolls Is first
briefly considered and a method of directly measuring the radial -00
04 easion of rolls Is de"loped. The derorration, or rolls .00
a owy r
pr"ased into contact is then dettermined by measurlnK the width or -00
the imprint an the lovmr roll made by the upper roll which was ."000
0 j t=00
coated with toot. Both static and dynamic experiment* wers,
:00 performed to investiKate tho deformation of the rolls when a strip COO
00.3
:00
of uniform thickness was plevoed or rolled botween them. In Vie
AVOW coo
lat*or case it was found that lateral spreading or them strip was cov-
00 000
fined to its edges owing to their &roster reduction in thickswes due
sea to the radial empressiov of the rolls. There is parabolic relation
9 between pressure and the radial compression of the rolls. ltvary-
1.091 0 0
thing which tends to increase the pressure an the rolls will cause an
Increase in the Irregularity of' the lateral distribution of the re.
4W A duation In thintm."Iss. This Irregulkatity id Iredujogby- joIlligii"fal,ed use
�Wk us~
1, iWtal and by"uslogismall reduotions por pass, polished rolls WA
~A Irsoo
I I A "FAWFAGOM CLASUPKATKII 11! C100
W114.0 NOW.
isiqvo o omv 4of
0 U0 AV 10 An I 1 4 PW 0 4 1 W 14 0 AD 0 ~I I
0 ev 0 a it 1111 011
of 0 a 0 0 of 0 0 41 0
0 0000*0 000040*000**000000*0 0
140- 0 0 0 of 01099 0 ofe, 0.00000 0 00 0 00000000 0 Is 0 0 of 0 : : 00 00 Of lot ii ,

*1* 0 see 0
a 0 a so's a 0 0 640 to a o 0 0 0 0 a c
4 9 It 11 11 it 11 14 if it U, ma", R N.
-j ad moot it it u to it to 10 u It w 0 pe
of I I'm to i j -%_t. I '-A
4r-
-00
al ~jp~j.KW Ma
00 'Ito, .114
- F, 1 -00
an, ptliah"l, wombed with IwAnol. AM ft-wral tin" sith hoot at.-r. TIm-y
ant then chirnmium-p6toM at W-47 V C. in chmmic arioll 2 to) Urm-litirr ml
:uIphurie &,.ut 2-2-8 pm./litn- at 15 Tloe llikkit.- of climinlin"I
Imouloll to 04Y.4 runt. After jdatinit. Ito- rt,11 -Imuld I.- fwaso,,l to, VAr V.
*or S.O.
3
zoo
41`1
00
zoo
boo
011TALLIMICKAL U1411411#041 Ct&IV#KAVIC%
19 a or t9 21tic ar "a A I AIN a 'i J3 a
goo go *I**** go 0 of *goo 00

Jill J3JJJI MD'All III It 12 1) w b )11 1) Is 1. w I u .1 4260
a I I AA IS CC UP U I I
L 6 R I I %I
00
:0
Lignovown bearings tor foiling mills. Va. S. (12IIAL
of or SJ41 0. N-- 4-5. 45 ('4e-. Zentr. 1939.;
-1.4111111"ll il P11.111-11 A' GIIIII.1: birch W's.1
12 1 ic-'~ ritlintur, i. t,,Iwd in ~Nw; ItIll,o- I~ g h_. j
0 A #I alm. and .101 !91'. pIv-l Illul" .791 at kg. .1. Coll.. -00
0 0 a Pt--1 AJ;4111 Ini-Irr 3:.1 in.
0 0 ntiprvCnAlVd Willi lliolkl,lite. Th,- fl,11-ming pmjwriie., at, Soo
00 -j,Kt-I I,ir Livl,-I-n .,nd Lign,if,l rt-Ii.: rv%j,lAncr ti,
7-W, Pk., And 1:91NI k4. -1. Von.; vvivil
0 0 4 friet, ... 1 11.1-11 41,111151 .111.1 11.14K1. '11. gr. L33 411.1 1 .;It; 400
00 -1.1; impAet rc,i,IAIICC lel) :!A -1.71111d :,'I
.4 vm. Vill.; &Jill vainicitv to ab%orh waier Ii and
06 o.2"r. ComparAtive limis on Trifolite. LignuOint and 17 COO
00 1.ml0fol ihojwril thc folletwing advaniage,; and disadvan-
to ISoo
aiges of tht. '21141 own prtiducts liver thr firm: a irrratrr
of vallacily for al-ohing wairr and lubricant. ' smater
0 0 S: rapar~fy fm IWI'Ilillg At ICUIP'. 21WJVC 11111% And lowrr re. :!-I roe
'iMLIn"i_ to COMP" ""'it. U19114111 114~ All th,, ;LdVAn1A9-
00 9 It..'s it~ d'_'ivjnIAJ,- Nt. 6. M goo
0
0 0 1 '00
'00
00
I noo
z
00 aftALLUROCAL LITEN.TUNt CLOSIFICATiC"
]too
-T- IF
_'F a PA L I a ad a 0 Is of I a v T
U
r prolt am Nit 41, Run IlwKwol 0 90060 0 0
0 0 0-0,0 0 0 0 0 a 0 0 0 0 * 0io 0 0 0 0 0 o 0 ;p 0 0 0 0 0 0 0 0 ei

C
-W~d
0
N;N00600000 a 0 0 W'; 0 0 0 Ill 0 9 0 0 0 0 9 0 0 0
0 13iI
4 I A 1 1 4
1 1 0 1 10 it 1) if it Is m 11 1 It At if 11 V it At It a 4 11 It 11 17 is
f,
A I It
V I
AA U 0 It lao m is to

00
[ I a 0 q
Q
,
t -A'. 1'. 0 t I
90
A

'LW=dOW 3Wjftp _jj~ SAN kjmL (Still. .00
A1139. No. 4-5, pp, 43-49). (11, Itumilill). Lignoidolle is limile 1)
drying birchwooil to a Mcialtulle -tent of 12-140." and thell
impregnating it under life at 90-(*)' C. with 420% glucotm-
m
"
r
-00
anil heat tri4atmentm.
b
several pr"ongs
solution, This is followfli
y
At
**
I
II- .
Filially the glucame with whieh the Wooij is illilletgliAtt4l i.14
iti
r it
immom of
j
l t
h .00
fee
, ' v
o un
e mater
a
clirillnellimixi by ImMing t
l
00 lj j~ mf 114) kg. per "q. cm. I IK*ton(, wan (11-v(,1411141 All a publititiltd.
l
l

go, a I
l : ling-mill 1~111g..
ite row um in ro
(or to-Mile.ninforml bakk

06 Is Ligumfol (plywouotl impregnated with bakelite) is another inatterial :3001

0 liropertien of tlx-Ae
developed for the some purpose. IMe ph)
0 two materials are daperibed =0 the design ofbearingo, the lubrication
*0 aml the results of works tests am dmk with. An compartlil with '00

o fabric-rvinfemml bakelite, lignoiltone halt a much lower loitiling 4111110,

" lifnit (715 kg. per s9. cm. as compared with 250-34K) kg. per Pq. cin.);
, 1:410 0
C. lignorol,
it has a tendency to swell at temperatures above 101.)
oil the other hand, is equivalent to fabric-reinforced liakelite. and it
chealwe matfrial.
.... . .. too
8 AETALLUROKAt LITINATill CLASUPICAPON [V.
W- TA
It a -It 411 lmi i
Witga it i a ftd a W 5 al
Ve 0 0 0 0 0 0 0 0 0 0 0 * 0 0 a 0 0 0 0 9 0 0 0 0 0 0 0 0 0 0 0

GAIMAf,--IAKCItSMnOVICH
Author:Oallai, !L4~v samuAlovich
Title: The lignitij Ierrous beavirgs. The Principles of Construction
and exploriiatiofi-- (Li nofolevyo i lignostonovye podshi rdk:l) Ij8 p.
3-P
City. Sverdlovalc
h&.1i.5hori
ctzt-- Scientific rnd -Technical Fifolication.
Da't--: 19116
Availablez of Comrcc-s
i*40TYthly Lizt cf,EL.-zi-71-a Accr:sssiom, 11,
ol. 3, 14a. 12~ ~10. 335

GALLAY, Ya. S.
PA 1FT34
UM/Vire - Drawing NRY 1947
Netallurgy
ngp I# Ta.
"The Theory of Multiple-dravn Wire by Slidi
S. Gallay., 6 pp
"Stall" Vol VII, No
The theory of multiple-draving of wire has noticeably
supplemented and improved the accepted foruvala for
designing draw plates. Also permitted the establish-
inent of a standard process and the greatest expansion
of diapason of the gap of the vIre-dra" vachinery.
Diagrams and formulae.
18T34

n -Ire

oft,
6 IS 0 0
jo 11 IS a V a it u is $d a x Lr x if a; It 41
OA..A
j L r. u. it I I-
00 A
0 Af
00
00
00
0
00
Z*L"duoj go- In awled maeowt. y"'s.
lotrilko%- and N -4 SAubwaki, A'trVimrr,,x I)jUrgt,
10. F$"(1. 1110, Tranniatt-a and coeult-titwtj
fe"'Ill NMI I. 194K. p. 37-Uk.
rpsults fo,r
all RM-10 nri- Ahown graphlrully aritl tlimcu&Rr,l.
00
00
ji
fi 4ETALLURGICIL CL *SUFICA71 00
St A
u fw 0 Pe
U sS 1.1 10 Ll! lp tee, Ign lilt olu It K pew
goo 0 0 goo 000 0000 0, q 0 04 0
-00
is
-0*
zo ID
We
moo
400
too

C,4
M~djWg of spaing of Ow w&W and oil absorption ad
wood V,4. $ QJIJ and M. A. Rudyk (Unin.
Itfad lust. i ziaraLWAIV livilro (lidromon.
cazlo. Za"skuvu Lah. 14. 949 minple
1.5 x 15 X 15 111131. of plmtk- 111"ll WAS tested for MA)
mlt~wption with neutral 11,0at SO' for Odays. Oil-lmx-p-
tion anti swrit-sis vmc dt(d. by using dittsydratid (91 at
50*Ior40-404ay%. The effects of temp. and at acid aad
%AAH -ddnt. to ihe IF,(.) site rrpcwtrl. O.V~ NaOll in.*
~r"ine ulmwptkm slightly aud OAV, 11'st). W"Itewhit
ni,we at %ta"IL'It Sit(ix

GALLAY, Ta. S.
Gallay, Ya. S. - "The treatment of high carbon steals from rolling heat," Sbornik
nauch.-takhn. rabot (Vaesoyuz. nauch. inzh.-tekhn. o-vo metallurgov, leningr. otd-
niye), Issue 1, 1949, p. 179-86
SO.- U-5240, 17, Dec. 53, (letopis 'Zhumal Inykh Btatey, No. 25, 1949).
1

QAT,TAY. Ya.S.. dotsent.
The use of wood plastics In the textile Industz7. Tekst.prom.
16 no.2:55-59 F 156. (MIJU 9:5)
(Textile machinery) (Woccl) (Metals. Substitutes for)

C L )AMU 1' 0 L)lc
ji
PH= I MM MIPMMATMY 601
Pavlov, Igor Nlkhaylovleh, jWM Takm ~am ov1ch, and Astakhov,
Ivan Gerulawrich
Rukovodstvo k ucbebnom laboratornam praktikvm po j?rdmtk* (YAmml for
Laboratory Course In Ho314 4ML3L Processes) 2d edo, reV. YANCOW, YAtal-
lurgIzdat, 195T. 5,000 copies printed.
Ed.: GolyatkIm, A. G.; Tech. Bd.: Attopar1chs X. K.
PuIWOSE: The book in Intended for students of metallurgical razes and for
sUidents in other fields taking a laboratory 'Course In "Ibtal Working by
Pressure",
COVERAGE: The book-diseusses the mthods; of canductiM a laboratory course In
mtal ro1ling and roll-dem1gm (except pro-rolllng)* Basle theoretical
J.nfoxmtion Is given and necessary =esuring devices and Instruments are
described. The work assignments in thin manual are coordinated with the
following tekt books:
Card 1/12

Manual for a Lsborafor7 (Ccut.)
6ol
1. Pavlov, 3g. M. The Theory of PALI-Ing and ftaftwntals of Plastic
Deformation., 2nd edition, Metallurgizdat, 1938.
2. Pavlov, Ts. M. - The Theory of Rolling (General PrInc1p;..'e 3f Metal
Morning by pressure). Netallurgizdat,, 1950.
3. Bakhtinow,* B. P. and Sbternovs, N. M..,Pm Design on F:jil Rolls,
Metallurgizdat 1953. There an no reference*
TABLE OF
CONTWRS:
Introduction 9
1. Pwpose of the sawisl 9
2. Emergence of rolling-mill training laboratories 10
3. State of ralling-odll training laborstasden In the USSR today 13
4. Methiods of teachIng In r*3'qng-*M trainInglaboratorles 18
Card 2/ 12

GILIFAND, Feliks Vullfovich; ALISHITS, Isaak Yakovlevich, kandidat
tekhnicheaki)da nauk; G T.T.IT T. jiw redektor; ARXHANGELISXATA.K.B.,
redaktor izdatellstvdw,~ tekhnicheskiy redaktor.
[Plastic-icoated bearing] Podshipniki, oblitsovannye plastmassof.
Noskya, Goo.nauchno-tokhn.isd-vo lit-ry po chernoi i tsvetnot
vietallurgit, 1957. 94 p. (KIRA 10:11)
I.Zavocl "Xras"y Vyborshots."
(Bearings (Machinery))

BILISKIY, B.11. [deceased]; BURIYANOV, 7.F.; VASIL'YEV, Ye.P.; VITKINA, R.I.:
GATJAY, U.S.; LEVIN, G.I.; MAIMYN, Yu.N.,-,. q*TUSTKIN, A.B.-
red.; ISTOMIN, A.B., red.; dldzflj~,a., red.:
NIFOOMSHCHIY, N.I., red. Izd-va; XARASAV, A.I.,-,.tbkhn. red.
[Ferrous metallurgy in capitalistic countries] Chernala metallurgila
Impitalisticheskikh stran. Ft,4.'[Rolling mill produotion] Prokatnoe
I tri'ibnoe p:roizvodstvo. Bellskii, B.A. and others. Moskva, Goa.
nauchno-tekan. izd-vo lit-ry po chernoi i tavetnol metallurgil.
195B. 627 p. (MIRA 11:7)
1. Moscow. TSentral'My nauchno-iseleaovateliakiy inatit-mt chernoy
matallurgii.
(Forging) (Rolling (metalwork)) (pipe, steel)

GALLAT. U.S., dota.
- -- - .. .11
"Rolling mill practices" by IU.M.Chizhikov. Reviewed b7 U.S.
Gallai. Izv.vys.uchib.zav.; chern.net. 2 no.6:161-166
Je 159. (MIRIL 13:1)
1. Severo-ZapadM-y zaochtV7 politekhaicheqIdy institut.
(Rolling (Motalwork)) (Chizhikov, IU.M.)

18. ouou
J, j,",
AUTHOR: GaJ luj, Ya. F). (DoCt~llt)
TITLE-' Review of the book "Ro.11ing Pi-oduction" hy Ghlzhjl~ov,
Yu. M., Second Revised and AmplIfU--cl EdiLlon, MetzL-
lL11'g1:!.dat, 1958, 61'-' pp. Y-10
PERIODICAL: Stall u ss ut
., 1959, Nr 10, PP 935-9-V
ABSTRACT: The reviewed book .1,, i,ecommu-ndod ;-A li~ltpdbook Po~-
metaIJAH-gical schoois but may LiLso be oC Luse to stud._--nts
of hiE.,;her learning and to enc-ineerr,s.
u
~ASSOCIATION: North Western Correspondence Polytechnic Inst- I 4Cute (Se%,.-
Zap. zaochnyy polit-ekhnIcheskiy institut)
Card 1/1

s/i37/6o/too/bii/bi6/04,3
AOO6/AOO1
Translation from: Referativnyy zhurnal, Metallurgiya, 1960, No.ii, p.116, # 26131
AUTHOR: Gallay, Ya.S.
TITLE; On the Friction Coefficient in Rolling
PERIODICAL: Tr. Mezhvuz. nauchno-tekhn. konferentsil na temut "Sovrem.dostizh.
prokatn. proiz-var, Vol. 2, Leningrad, 1959, pp. 391 - 392
TEXT; Simultaneously with investigations of the magnitude of friction
forces in rolling, the problem is set on the necessity of continuing the study of
physical phenomena occiirring at the contact surfans (the process of destruction
and impression of scale, etc). These phenomena affect considerably the nature of
the distribution of friction forces, the quality of the rolled stock surface, and
the wear of the rolls.
B.Sh.
Translator's note., This is the full translation of the original Russian abstract.
Card 1/1

N /f I-r i
Vlyl V
PHASE I BOOK EDIPWITATION SOV/4420
Materialy po teorii prokatkiY ch. VI (materials on the Theory of Rolling, Pt. 6)
Moscow, Metallurgizdat, 1960. 496 P. 3,250 copies printed.
Compiler: Yakov Samuiloy~g"&U�y_, Docent; Ed.: 1g. M. Pavlov, Corresponding
ae-
Member, Aca my Ff Sciences USSR; Ed. of Publishing Howe: L.M. Gordon; Tech. Ed.:
M.K. Attopovich.
PURPOSE: This book is intended for scientific research workersY aspirants., and
technical personnel of metallurgical and machine-building plants. It may also
be of use to students of schools of higher technical education and tekhnikums.
COVER,hGE: This is part six of a multivolune series covering materials pub-
lished frm 1933 through 1956 in the Soviet Union and other countries on the
theory of rolling of metals and an the results of experimental in7estigations of
certain problems connected with this process. Part six contains materials pdb-
lished in the period 1946 - 1956 on the kinetics of metals in cold and hat roll-
ing, forcee acting between the work and the rollsY distribution of pressure over
the arc of contact,, effect of the speed of rolling on deformation resistance.,
elastic deformwtion of a mill caused by pressure of rolling, consumption of
Card 1/8

Materials an the Theory of Rolling, Pt, 6 SOV/4420
ener&w, determination of torque, and on the influence of rolling speed and ten-
perature- en energy consumption. No personalities are mentioned. There are
362 Soviet and non-Soviet references listed by chapters.
TABLE OF OTTERS -.
Principal Symbols Used in the Text
Ch. IV.. Forward Slip, Backward Slip, No-Slip
6
1. B.P. Bakhtinov's formula for forward slip (1946) 7
2. Forward slip formula with consideration of spread (1g.M. Pavlov,1947) 12
3. Forward slip in rolling with tension (Yu.M. Faynberg, 1948) J8
4. Formula for the neutral angle with consideration of spread (A.P.
Chelmarev., 1948) 21
5- Slippage and forvard slip In rolling in Laut's nftli (1.D. Kuzema,
1950) 30
6. Forward and backward slip in rolling between grooved rolls
(I.M. Pavloir., M.I. KapustinY 1950) 37
7. Calculation of forward slip in cold rolling (R.B. Sims, 1952) 53
8. Forward slip in rolling with (me friction-dxiven roll (W. Lueg,
K.H. Treptor, 1955) 59
caxd 2/8