SCIENTIFIC ABSTRACT ZHABREV, I.P. - ZHABOTINSKIY, S.N.

• Document Type: CREST
• Collection: Scientific Abstracts
• Document Number (FOIA) /ESDN (CREST): CIA-RDP86-00513R001964520007-7
• Release Decision: RIF
• Original Classification: S
• Document Page Count: 100
• Document Creation Date: November 2, 2016
• Document Release Date: September 19, 2001
• Sequence Number: 7
• Publication Date: December 31, 1967
• Content Type: SCIENTIFIC ABSTRACT

YEGOYAII, V.L. Etrsnslatorj;-~ ~-I.Pjtransiatorj; KOLCHANOV, V.P.
'[translator]; MOISMVA, T.K.Ctranaiatorl; PMTWO,V.S.
(translator]; PETRENKO, I.K. (translator]; SrRUKOV, N.-D.
(translator]; TITOVA, N.A. [translator];-MINO V.Ye., red.;
ROMAITOVICH, G.P., red.; REZOUKHOVA, A.G., tekhn.red.
[Present-day studies of the tectonics of foreign countries)
Voprosy sovremnnoi zarubezh~oi tektoniki; sbornik statel.
Moskva, Izd-vo inostr.lit-ry, 1960. 498 p. Translated articles.
(MM 13:12)
(Geology, Structural)

GROSSGEYM, V.A.; YEGOYAN, Y.L.; Z9411m, I.P.; SURDANOV, A.N.
"Structural geology" by G.D.Ar-bgirei. Reviewed by YJ..
Grosegeim and otbers, Izv*v7s,uaheb.zav.; geolei rezv.
no.3.'136-139 MY 160, (MIBA 230
1. Krasnodarskiy filial Voesoyuznogo nauchno-iseledovatall-
skogo inatituta nefti.
(Geology, Structural)
(Azhgirei, O.P,)

ZRAMM, I.P.
Oil and gas-bearing prospects in the eastern part of the Azov region.
Geol.neftl I no.10:16-20 0 '57. (MIRA 10:10)
1. Kraonodarskiv filial Vuesoyuznogo neftyanogo nauchno-iteledovatelookogo
instituta.
(Azov region--Petroleum geolog7) (Azov region--Gas, Natural--Geology)

KHAIN, V.Ye.; SHAMMY , I P.
Role of dispir folds in the tectonics of southeastern Caucasu4.
Trudy Inst.geol.AN Azerb.SSR 15:~-58 '54. WaA 9:1)
(Caucasus--Geology, Structural)
MIX
1114,11 W
Ito

ZHABREV, I. P.
"Characteristics of the Tectonics of the Central Part of
Eastern Kobystan Northwest Apsheron." Cand Geol-Min Sci, Inst of
Geology imeni I. M. Gubkin, Acad Sci Azerbaydzhan SSR.. 13 Nov 54.
(BR, 3 Nov 54)
Survey of Scientific and Technical Dissertations Defended at USSR
Higher Educational Institutions (11)
SO: Sum. No-521, 2 Jun 55

(Krasnodar Territory--Petroleum geology)
(Krasnodar Territory-Gas, Natural-Geology)

ZHABLEV, I.P.
Some problems of the'history-of the geological development
of Ciscaucasia in the.Mezozoic and-Cenozoic. Trudy KF
ViffI no.10:1?7-184 162a (HIRA 15:11)
(Caucasus, Northern-Geology)
WN NAROMM LT-1~iil-4~ma;_~mav~,~.a-lw-g&%RB&M Rum wldsd~- -AWNIMM,

ZHMEVO I.P,;,DVORTSOVA,, A.A.
Types ofiD:Ll and gas.pools in Miocene sediments in the
ocuthern edge-of the western Kuban marginal_-6!6ugh and
methods of''prospecting for them. Trudy V VIIII no.10:19-A".7
162. (MIRA 15:11)
(Kuban Lowland-Petroleum geology)
(Kuban Lovland-Gaso.Natural--Geology)

ACC NR1 AP6029745 SOURCE com: UR/0210/66/000/005/0021/0029
AUTHOR: Zhabrev,_ I..---P.
ORG- Krasnodar Branch, All-Union Oil and Gas Scientific Research Institute
(Krasnodarskiy filial Vse6oyuznogo neftegazovogo nauchno-issledovatel'skogo
instituta)
TITLE: Some problems in the use of mathematics in geolo
SOURCE: Geologiya i geofizika, no, 5, 1966, 21-29
OPIC TAGS: mathematical modeling, geological model, stochastic,.model, information
heory
f
ABSTRACT: Using logical and mathematical methods, possible st~'cihastic no els are
developed for the quantitative description of the boundaries of geological bodies
-and objects. These models are based on bnalogous ones of material objects described'
by I. A. Achkurin -[Teoriya elementarnykh chastits i teoriya informatslya - Sb. Filo-
sofskiye probl. fiiiki elementarnykh chastits. M. IL, 1963) as created in, informa-;
tion theory, programming, and automation. The'applications of the simplest models,'; ,
those associated with information theory, to geology are described. Computations
are made to determine the information required for one atom in different rock types,','
and ways are explored to eliminate unnecessary information. The possibilities of
correlating geological sections on the basis of the information theory and of

J, h69)dj-66
ACC NR: AP6029745
employing computers in these operations are examined. Orig. art. has: 2 tables and
3 formulas. (DM]
SUB CODE: 08/ SUBM DATE: 23Mar64/ ORIG REF: 009/ OTH REF: 003/
Card 2/2

Nutrition of the cod in shore waters of the Eastern Muman Coast.
Tirudy Harm. biol. sta. 3.-14o-147 157. (MIRA 11:2)
(Hurmn Coast--Codfish) (Fishea-Pood)

Lithologic and petrogr aphic characteristics of Albian
sediments in western Ciscaucasia. Trudy KF VNII
no.10:195-206 1,62, (MIRA 15:11)
(Caucasus, Northern-Rocksp Sedimentary)

ZHAWZVA, P.S.
Gone-in-cone structures in Lover Crataceous sediments of tha north-
western Caucasus. Trudy XF VIIII no.1:237-242 159. (I-aRA 16:!?)
(Caucasus, Northarn-Petrology)

Carbonate rocks in Cretaceous sediments of the northvestern Cauca-
sus. Trudy KF VNII no.6;2Z2-233 "61. (MM 15.2)
(Caucasus, Northern-Rocks, Carbonate)

VASILITRA, V.Ta,, otv,red,; GIJBIR, A.A., otv.red.; UZTAWV, A.N.. otv.rado;
ZRABREM, A.F,, red,; VASILITW, red.;-IPSHT3TN,-V.G., red.
-WrtYT-MMM, Ta.L., red.ikd-va: FR3MLI, M.Yu., red.isd-va,,
PAITASOYARTS, M.D., red.izd,7'va; TSIGELIMAW, L.T., tekhn.red.
(Union of Burma; a collection of articles] Birmaniskii SoWs';
sbornik statel. 14oskva, Ind-vo vostochnoi lit-r7, 1958. 291 p.
(MIRA 12:2)
1. Akademiyaj2auk SSSR. Institut vostokovedonlya. 2. Naucbm7
sotrudnik Instituta',~ostokovedeniya-(for Spahteyn).
(Burma)
w I Egli,
"OMNI.; v I ~~~
-IM
-2 WON MORT
= I W-1 4111 MY 10"M W SIMPI'M

MIMYEVA, 09N.; ZHABRONOVA, Z.A.LPOPOVA. L.A.; X&MENSKIY, I.M. [deceased];
BELIKinuo M.G.; TSVRWA, I.A.; SMOLINATA, L.M.; KOTKOVA, M.P.;
USHITSYNA, A.D.
Blosynthesis of tetracycline on enriched media. Ked.prom. 14
nQ,It3!-!34 Za 160, (MIRA
1. Xoskovskiy zavod meditsinskikh.preparatov 16.1 1 T8aqOYuzu37
nanchuo-issledovatellskly institnt antibiotikov.
ITZMCYCLINI)
M~I- MWORM MERUMVIM NWSIRMVII--~- WMM

P11 1GT88
ZURMV A.
'
USL
8R
OPU3:10106:~ Feb 1947-
Aircraft PropUlej OM
"Jet Propelled Aviation," A. Zhabrov, 2 pp
"Za Oboronu" Vol XXIII, No 3
Discusses siibJect on popular le*el. Principle of
operation explained. Types of Jet prcpulsion engines
discussed.- "Shooting Star" and "Air CCMet"L perf or -
mance discussed kwith photographs). American-British
conference on jet propulsion and gas turbInes in
1945 is mentioned.
ioT88L

ZHABRO MIKIRNMOV, X.,. redaktor; BZLYAKOV, A., tekhnicheekly re-
W,
t or.
[Airplanes, gliders, autog~ros, helicopters] Samolet, planer,
avtozhir, gelikopter. Koskva, Redizdat US Soiuza osoaviakhim
SSSR, 1948. 192 p. [Microfilm] (KLRA Ba)
(Airplanes) (Gliders (Aeronautics)) (Autogiros) (Heli-
copters)
t 0 HE

PANKOV, M.I.; !!!!!&,,~daktor; ENLYAKOV, A., tekhnicheskiy redaktor
[Work of the model airplane club] Rabota aviamodellnogo Icruzhka.
Moskva, Itedizdat ToS-Soiuza osoaviakhim SSSR, 1947. 125
[Microfilm) (MA gal)
(Airplanes--Xodels)
"1111 SPIN R-01-11TROW-W

-Zhabrovi-A:Leksel-Alelcsandrovieb-,~--
The theory and practice of fli-ht. Foskva, Redaktsionno-iz-datellskil otdel
Aeroflotal 1948. 483 p. (49-.15782)
TL.5?0.Z3

V4
R.:
to
?I

ZHABT-W, JILEYSE1 ALEKSANDROVICH.
Tporiia i teklmika poleLa; prakticheskniti aprodinamika. Chast'l. Qsnovy
poleta namolcta. Moskva, Izd-vo Dosam, 1950. 191 p., illus., -orts.
Title tr.: Theory and techiiique of flying. Applied aerodynamics.. Part I.
Fundamentals of flying of 3ircraft.
TL570-Z32
SO. Aeronautical Science and Aviation in the Soviet Union. Library of
Congress, 1955.

"The Airplane Glider, Autogiro and Helicopter.," P. 314) 1952.

ZFIAIMOV,A.
Gyroocopic effect of the propeller. Kryl.rod. 2 no.10:
21-22 0 '51. (KWA 8:8)
(Propellers, Aerial)

PHASE I BPOK EXPLOIMATION SOV/3782
Zhebrov, Aleksey Aleks-androvich
Teoriya poleta i pilotirovaniya samoleta (Theonj of Flight and Pilotiog of
Airplanes) Moscav., Izd-vo, DOSAAF., 1959. 411 p. Errata ollp innertsd,
10,2D0 copies printed,
Ecb.: A.A. Vasillyev,, and V.I. Fedorov; Tech. Ed.: M.S. Karyakina,
PURPOSE: This ,is a textbook for self-instraction. of students and yongg pilots.
COVERAGE: The textbook conforms vith the program of USSR aeroclube for tesebing
the theory of flight and piloting of propeller aircraft. The book also gives
a brlef,~utline of the theory of flight and piloting of jet planes. Basic
aerodynamics, aerodynamic characteristics of aircraft, pover plants, various
regimes of aircraft flight, stability and maneuNmrability,.-acrobatic flight,
and maneuvering characteristics of the Mig-15 bis airplaneare discussed. The
author used material from books by V.S. Pyshnov, I.V. Ostoslavskiy, V.F. Bolot-
nikov, B.T. Goroshchenko, P.M. Shirmanov, B.N. Yurtyev, N.A. Zaks, A.K. Martynov,
and Ya.l. Levinson) and also from official publications on the aerodynamics and
piloting of the Yak-18, Yak-11, and Mig-15 bis airplanes. There are no references
Card 1/ 14

Theory of Flight and Moting of Airplanes SOV/3782
TABLE OF CONTMS:
Introduction
PART I. THHOBY OF FLIGM AND PI10MG OF PROPELLER AIRM.FT
Ch. 1. Air and Its Properties 9
1. Earthts atmosphere 9
2. Air temperature. Absolute temperature 11
3. Air pressurei, Decrease of pressure with altitude
4. Air density. Density as a function of pressure and temperature 13
5. Standard atmosphere 1T
6. Viscosity of air 19
T. Compressibility of air 19
Ch. II. Basic Laws of Air Flow 20
8. Air flow and principle of revers ibility. Wind tunnel, Steady flov 20
9. Laminar and turbulent air flows. Boundary layer 23,
10. Equation of continuity 25,
11. Static pressure in the flow and dynamic pressure 2T
12. Bernoulli's equation 28
13. Velocity measurement of an air flovVelcicity coefficient of an aircraft 30
Card 2/14

Theory of Flight and Piloting of Airplanes sov/3782
Ch. 1 27. Aerodynamic Forces 33
14. Air drag. Air flow about liodies 33
15. Basic law of air drag 34
16. Symmetrical flow and source of drag force 36
17. Aerodynamic drag coefficients of various bodies and non-loadcarrying
components of aircraft 38
Unsymmetrical flow-and generatian or total aerodynamic force 41
Ch. IV* Aerodynamic Characteristics, of Wings 43
19. Wing of.an aircraft. Incidence angle and angle of attack of a wing 43
20. Formation of the lifting force of a wing. Pressure distribution
along the wing*. 49
21. Aerodynamic forces on a wing., their coefficientsj, and relationships
between theza 52
22. Aerodynamic coefficients as functions of angle of attack and vJj4;
shape 54
23. Aerodynamic efficiency of a wing. Angle of maximum efficiency 56
24. Drag of a vingi Profile drag and induced drag 58
25. Aerodynamic testing of wings. Polar of a wing 62
26, Adding flaps to a ving (methods 43f increasing maxlymun lift force) 67
Card 3/114

Theory of Flight and Pilorting of Airplanes SOV/3782
Ch. V. Aerodynamic Characteristics of Aircraft 71
21. Lift.-force and drag of an aircraft 71
28. Polar of an aircraft 73
29. Aerodynamic efficiency of an aircraft. Methods of increasdng
efficiency 76
30- Effect of sideslip of an aircraft on lift force and efficiency 79
Ch. VI. Power Plant 82
31. Purpose of th e power plant and general information on propellers 82
32. -N,,ometrical characteristics of a propeller4- Effective pitch and
.Propeller slip 84
33. Angle of attack of a bleide element and its.dependence on trans-.
lational and circumferential velocities 88
34. Thrust and resisting torque of a propeller and regimes of its
operation 91
35. Propeller thrust as a function of aircraft speede Effect of altiVide
on propeller thrust 94
36. PropeUer resistance moment and engine torque 95
~7, Useful pover and efficiency of the propeller and their dependence on
aircraft speed. Effect of altitude on power-plant output 96
38. shortcomings of propellers of Invariable or fixed pitch. Variable-
pitch propellers and their advantages 100
Card 4/ 34

Theory of Flight and Piloting of Airplanes sov13782
39. Working principle of a hydraulic propeller 103.
40. Working principle of an aeromechanical propeller 106
41. Feathering, reversible., and coaiial propellers 110
42. Contribution of Soviet scientists to the development of propeller
theory 111
Ch. VII. Horizontal Flight of an Aircraft 112
43. Conditions of equilibrium of forces in horizontal flight. Wing
unit loading 113
44, Velocity required for horizontal flight 115
45. Effect of angle of attack on necessary velocity. Inclination of the
airplane toward the,horizontal at various speeds and maxim= speed,
Minimum speed 115
46. Thrust required for horizontal flight 119
47. Required thrust as a function of aircraft speed (Zhukovskiy's curve).
Necessary and available thrusts 121
48. Power required for horizontal flight 125
49. Required power as a function of aircraft speed (Zhukovskiy's curve).
Required and available power 127
50. First and second regimes and velocity range of horizontal flight 130
Card 5/ 14

Theory of Flight and knoting of Airplanes SOY/3782
51. Effect of altitude on required speed. Altitude instrument readiag*
Instrument speed., indicated and true flight velocities 132
52- Effect of altitude on required power. Required and avail6le pover
at altitude 136
53. Effect of wing loading on flight characteristics of an aircraft In
horizontal flight 141
54. Eff eat of wind on horizontal flight 143
55. Work of Soviet scientists on aerodynamic calculation and dynamics
of aircraft 145
Ch. VIII. Climb of an Aircraft 146
56. conditions-6f equilibrium of forces in climb 146
57. Velocity required for climb 147
58. Thrust required for climb 148
59. Angle of climb and inclination of the aircraft toward the horizaital
in climb 149
60. Power required in climb and vertical climbing speed 151
61. Tndicative curve of climb trajectories. First and second regimes
of climb 153
62. Effect of altitude on vertical speed., ceiling, and rate of climb
of an aircraft 156
63. Effect of wind on climb 16o
Card 6/ 3,4

Theory of Flight and Piloting of Airplanes SOV/3782
Ch. IX. Gliding of an Aircraft 162
64. of equilibrium of forces in gliding. Diving
Conditiono 162
.
65. ,
Gliding speed. Limiting speed of an aircraft 164
66. rizoatal
Gliding angle and inclination of the aircraft toward the ho
, ,
in gliding 166
67. Vqrtical gliding,speed
68. Indicative curve of gliding trajectories. First and second regimes
oT gliding
69. Gliding range (in the absence of wind). Time of gliding 172
70. Effect of vind on gliding 174
Ch. X. Equilibrium,, Maneuverability., and Stability of an Aircraft 179
71. Aircraft equilibrium in flight (general: concept). Axes of rotation
9ments of forces
1
of the aircraft and n 179
72. .
.
Center of pressure of a wing. Mean aerodynamic chord 181
73. Gravitational center of an aira=aft
74. Centering of an aircraft and its recalculation .185
75. Iongitu Idinal equilibrium of an aircraft 188
76. Effect df wing moment on longitudinal equilibrium 191
17. Effect of horiznntal tail assembly moment on longitudinal equilibrium 194
Card 7/14

Theory ofFlight and Piloting of Airplanes SOV/3782
78. Effect of pover-plant moments 'on longitudinal eqmilibijum 196
79. lateral equilibrium of an aircraft. Effect of reaction of propaller
rotation on lateral equilibrium 199
80. Directional equilibrium of an aircraft, Effect of propeller slip-
. stream on directional Oquilibrium 200
81. General concept of aircraft maneuverability 203
82. Longitudinal Ymneuverability of an aircraft. Action of the Clevator.
Balancing curve. ,Degree of maneuverability 203
83. Effect of the position of benter of gravity of an aircraft Ion its
longitudinal maneuverability 207
84. Methods of reducing pressure on the control stick. Acirodyneoic
compensation of the elevator. Trim tab 208
85. lateral and- directional -neuVerability of an aircraft. Action of
ailerons and the rudder 21-1
86. General concept of stability of an aircraft. 215
87. Longitudinal stability. Acrodynamid center. Center of litt of the
aircraft and dependence of stability on the position of center of
gravity 216
88. Manifestation of stability in flight = .
89. Lateral and directional stability of an aircraft 223
90. lateral damping of vings 226
Card 8/34

Theory of Flight and Piloting of Airplanes SOV/37132
Ch.. XI. Take-O,,ff and Landing 2Z,'
91. Take-off of an aircraft (general concept). Take-off stages and
take-off distance 228
92. Ground run of an aircraft and aeparation from the ground. Accele-
ration during ground run. Separation speed 229
93. Leveling-off of an aircraft to pick up speed. Take-off speed and
climbing stage 232
94. Normal take-off and take-off errors. Restrictive take-off (abrapt
termination of take-off run). ~Take-off with loy tail 233
95. Calculation of length and time of ground run and take-off d1staace
(in the absence of wind) 236
96. Effect of veight, and other factors on length of ground run imd 'take-
off distance 239
97. Effect of vind on take-off. Take-off in a cross wind 240
98. Landing of an aircraft (general concept). -Landing stages 245
99. Calculation of landing. Error in the calculation of glidir*,, range.
Methods of reducing gliding range 246
100. Trimming of an aircraft. Leveling offj, landing., and landing rwi ~252
101. Landing speed and methods of reducing it. Types of landing and
errors in landing 255
Card 9/114

Theory of YUght and Piloting.ofAirplanes SOV/3782
102. Length of landing ran and calculation 9f landing distance (in the
absence.of vihd) 258
103. Effect of vind on landing. -landing in a cross wind 26o
'Ch. XIL Turns and S~~s 262
104. General concept of curvilinear flight. Effect of gyroscopic montent
of the propeller. Aerodyqamic load factors 262
105. Turns. Correct turns) action of forces 268
106. Radius of tu= and its dependence on flight speed and angle of bank,
Time of a turn. load factors in turns 270
107. Speed in turns. Turning errors 275
108. Thrust and pover required for turns. Turns vith maximum efficiency 278
109. Control of aircraft and operation of rudders in correct turns 279
110. Incorrect turns vith sideslip 283
M. Spiral, action of forces and speed in a spiral. Most efficient
spiral 2B6
Ch. -Xin. Spin of an Aircraft 288
112. General information on spins. Danger of invbluntary spin at low
altitude 288
113. Principles of spin. Autorotation of wing. Rotational moments iia spin 292
Card ID/ JJ4

Theory of Flight and Piloting of Airplanes Sov/3782
3.14. Effect of position of center of gravity and other factors on spin
characteristics 296
115. Characteristics of spin regimes 298
116. Placing an aircraft into a spin and pulling it out. Effect of
ailerons and pover plant. Load factors in spins 299
Ch. XIV. Acrobatic Flight 303
117. Purpose of acrobatic flight. The role of Soviet fliers in the
development of acrobatic flying 303
118. Nesterovts loop [Norn~ai loop]. Action of forces and speed inthe
loop. Performance of a loop 307
119. Steep climb after take-off. Action of forces and performance; of
the:steep climb 312
120. Combat [climbing] turns 313
121. Pushing over into a nose dive and pulling out of it. 1,oss of
altitude in pulling out 315
122. Wing-over with spin and controllable ving-over 318
123. Nesterov's halfloop (Immelman turn] 322
124. Turn in a steep climb 323
125. Inverted flight 324
Card 11h.4

Theory of Flight and Piloting of Airplanes SOV/3782
PART 11. SPECIAL FEATURES OF TMW OF FLIGHT AND PIZM33G OF JET XTRCRAFT
Ch. X7. 4sic Aspects of High4 peed Aerodynamics 329
126. Compressibility of air. Speed of sound. Mach number 329
127. Propagation of sound vaves in an airflow 333
128. Flow of a supersonic air stream about bodies. Shock Vave aneL Vave
drag 335
129. Drag rise of near-sonic speeds. Criticial Mach number 338
Ch. SVI. Aerodynamic Characteristics and Types of High-Speed 400 4iraeaft 340
130. Pi~6ssure distribution along the airfoil of the ving at hypercwitical
Mach numbers 340
131. Variation of aerodynamic coefficients and quality of the vine: as
functions of the Mach number 341
132. Polar of a jet aircraft, its lift force and drag 3114
133. Aerodynamic forms of high-speed jet aircraft. The Mig-15 bis air-
,plane 346
134. Propellers for high-speed aircraft 351
135- Contribution of Soviet scientists to the development of aerodyawlics
of high speeds and of high-speed aircraft 352
Card 3~/114

Theory of Flight and Piloting of Airplanes SOV/3782
Ch. XVIL Power Plant of a Jet Aircraft 354
136. Jet engines (general concept). Air-breathing jet engines (VIM) 354
137. Turbojet engine (m) 357
138. Thrust and thrust power of turbojet engines. Effect of flight
speed and altitude on thrust of turbojet engines 359
Ch. XVM. Rectilinear Flight of a Jet Aircraft 362
139- Thrust required for horizontal flight and its dependence on the
Mach number 362
140. First and second regimes and velocity range of horizontal flight 364
141. Acceleration and deceleration in horizontal flight 367
142. Speed in climbj, angXe of climbj, vertical velocity, ceiling., Cind
rate of climb 369
143. Descent with engine running) gliding., and nose dive 371
144. Restrictions with respect to speed and Mach number. Flight blach-
number index 373
Car5d 13/14

Theory of Flight and Piloting of Airplanes SOV/3782
Ch. XIX. Stability and Maneuverability
145. Longitudinal stability and maneuverability
146. Forces on the control stick transmitted by the elevator in
rectLI-inear flight at hypercritical Mach numbers
147. IncreAse of forces for producing unit over load faetor
148. Lateral and directional stabilityand maneuverabi-lity
149. Reduction of effectiveness of ailerons. Wdraulic amplifier
(booster) and internal compensation of ailerons
150. 14voluntary banking of an aircraft ("Irregularrolling")
151. Reverse reaction of aircraft for deflection 6f the'rudder
Ch. XX. Take-off and Landing
152. Take-off of jet aircraft
153-~ Landing and -landing speed. Landing vith cross wind
Ch. Ma. Spin and Acrobatic Flight
154. Spinning of the Mig-15 bis airplane. Execution of spin
155. Maneuvering characteristics' of the Mig-15 bis airplane
156. Simple and complex pilotingt,,
Appendix: Greek Alphabet
Ann~wm Library of Congress
fCard lh/14
375
375
376
380
380
38P
383
385
387
~89
393
393
396
398
404
AC/mg
6-21-60

NAME
7'
ZHABROV) ALEKSE( ALEKSAYDROVIC.H.
Annotirovannyi ukazatelf literatury na russkom iazyke po aviatsii
i vozdukhoplavaniiu za 50 let, 1881-1931. Teoriia. Tekhnika. Stroitel'stvo.
Ekonomika. Statistika. Istoriia. Mirnoe primenenie. Moskva, OTITIJ
NKTP SSSR, G~s. aviat. i avtotrakt izd-vo, 193). 312 p.
Title tr.: Annotated bibliography of litbrature in the Russian
language on aviation and aeronautics for 50 years, 1881-1931. Theory.
Technology. Construction. Ecoromics. Statistics. History. Peace-
time aviation.
Z5065.R9Z6
SO: Aeronautical Sciences and Aviation in the Soviet Union., Library of
Congress, 1955.

ZPABRGV, ALMEY JkLIEKSANDROVICT.I.
Pochcmu i kak letaet avtozhir. Moskva, Glav. red. nouchno-popul.
i iunosh. lit-ry, 1936. 174 P., illus., diagrs.
Bibliography; P. 172.
Titletr.: How and why an autogiro flies.
TL715-Z5
SO: Aeronautical Sciences and Aviation in the Soviet Union, Library of
Congress, 1955-
W
M
MMMMOMI-M MWOMM

ZTIABROV, ALEMEI AI,7.KSANDHOVTCII.
Kak i pochamu letaet planer. 2, izd., inopr. i dop. Moskva,
Glav. red. nauchno-popul. i iunosh. lit-ry, 1938. 203 p-, illus.,
diagrso
Title tr.: Pow and why a glider flies.
TL760.Z46 1938
SO: Aeronautical Sciences and AvLation in the Soviet Union, Library of'
Congress, 1955.

gig mm=zimjmmawm~
f 1
MABROVI ALEKSJ ALEKSANDROVICH.
Teoriia i tekhnika poleta, Moskvaj Redaktsionno-izdateliskii otidel
Aeroflota, 1948. 483 p., diagra.
Bibliography; P. 478.
Title tr.: Theox7 and technique of flying.
TL570.Z3
SO: Aeronautical Sciences and Aviation in the Soviet Union., Library of
Congress, 1955.

-OV
HABR p AIEKSE ALENSANDROVICH.
Z
Teoriia i tekhnika poleta; prakticheskaia aerodinamika, ChaBt'I. 0snory polota sawlata
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(Why and how an airplane flies] Pochemu i kak letaet samolet.
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w m P Me,

BMW.
ZHABROV, Aleksey Aleksandravi6h; VASILIYEV, A.A.,rea.; FEDOROT, T.I.,
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[Theory of the flight and piloting of an 'airplane] Teoriia,
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ZHABROV, A.B,. inzh.
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