Крылья
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Численное решение задач внешней аэродинамики : учебно-методическое пособие для студентов естественно-научных дисциплин
2016
511
293
247
A theory of the blockage effects on bluff bodies and stalled wings in a closed wind tunnel
1965
1693
16
7
Aspects biochimiques de la différenciation des disques imaginaux alaires des Lépidoptères : Thèse prés. à l'Univ. Paris VI
1975
2596
130
103
Theoretical pressure distributions on wings of finite span at zero incidence for mach numbers near 1
1961
759
64
50
An experimental investigation of the subsonic longitudinal characteristics of five slender-wing models with gothic planforms
1973
1503
338
312
Сравнительные экспериментальные исследования отрывного обтекания прямых крыльев с гладкой и волнистой поверхностью
2002
2904
77
62
Calculated spanwise lift distribution and aerodynamic influence coefficient for unswept wings in subsonic flow
1953
800
146
121
The application of a parametric method of fatigue load measurement to wings - based on flight measurements on a lightning Mk T5
1979
1687
339
322
Аэродинамика : учебник для студентов высших технических учебных заведений. 1 : Основы теории. Аэродинамика профиля и крыла
1976
2949
426
403
Low-speed aerodynamic characteristics of NACA 0012 aerofoil section, including the effects of upper-surface roughness simulating hoar frost
1973
2066
321
258
Effects of finite span on the section characteristics of two 45° sweptback wings of aspect ratio 6
1953
2166
87
72
Measurements of lift and ground interference on a lifting-fan wing at zero forward speed
1962
1684
212
187
Measurements of pitching oscillation derivatives at subsonic and transonic speeds for a cropped delta wing of aspect ratio 1,8 : (Interim report)
1961
657
494
546
Effects of Reynolds number and frequency parameter on control-surface buzz at high subsonic speeds
1972
2061
78
60
Effect of high-lift devices on the static-lateral-stability derivatives of a 45° sweptback wing of aspect ratio 4.0 and taper ratio 0.6 in combination with a body
1952
1550
306
247
Феногеография крылового рисунка Polyommatus icarus (Lepidoptera, Lycaenidae) : Автореф. дис. на соиск. учен. степ. к.б.н. : Спец. 03.00.09
1992
1279
345
328
Upwash interference in a rectangular wind tunnel with closed side walls and porous slotted floor and roof
1963
2288
482
395
The geometry of wing surfaces generated by straight lines and with a high rate of thickness taper at the root
1958
1516
321
290
Wind tunnel measurements of the low speed stalling characteristics of a model of the Hawker-Siddeley Trident 1C
1969
2472
203
162
Free-fight measurements of the zero-lift drag of a slender ogee wing at transonic and supersonic speeds
1964
941
177
156
Quasi-cylindrical theory of wing-body interference at supersonic speeds and comparison with experiment
1955
1362
484
427
Wing flow measurements of the damping in pitch derivative of a 45° delta wing-body combination and with a tailplane in two positions
1958
2210
156
129
The effect of temperature variations in the plane and through the thickness of a circular lenticular plate
1962
1235
451
379
Аэродинамические компенсации шарнирных моментов рулевых поверхностей самолётов с ручным управлением : справочник
2017
1970
23
14
Корабли и суда на подводных крыльях : основные конструктивные типы отечественных кораблей и судов на подводных крылья, 1915-1955 гг. : монография
2014
990
459
409
Charts and approximate formulas for the estimation of aeroelastic effects on the lateral control of swept and unswept wings
1953
565
90
101
Longitudinal stability characteristics of low-aspect-ratio wings having variations in leading- and trailing-edge contours
1964
2257
290
242
Pressure measuremenst at the centre of a 40° swept back wing with R. A. E. 101-10 sections at zero incidence and transonic speeds
1961
1658
298
278
Recherches sur la morphogenèse et le polymorphisme alaire des Blattaria : Thèse prés. à la Fac. des sciences de l'Univ. de Rennes ..
1969
2822
44
31
The centre section shape of swept tapered wings with a linear chordwise load distribution
1960
2182
444
428
Gun tunnel measurements of lift, drag and pitching moment on a 20⁰ cone, a flat delta and a caret delta wing at a mach number of 8.3
1966
1322
172
140
A comparative examination of some measurements of airfoil section lift and drag at supercritical speeds
1952
2686
121
104
Area-suction boundary-layer control as applied to the trailing-edge flaps of a 35° swept-wing airplane
1958
1224
75
61
Effect of ground interference on the aerodynamic and flow characteristics of a 42° sweptback wing at Reynolds numbers up to 6.8×10⁶
1955
1124
244
214
Measurements in flight of the longitudinal stability derivatives of a 60° delta wing aircraft (Fairey Delta 2)
1963
1609
422
361
Колебания и устойчивость упругой полосы в сверхзвуковом потоке газа : Автореф. дис. на соиск. учен. степ. к.ф.-м.н. : Спец. 01.02.04
1995
1813
381
326
Численное исследование вязких течений на многопроцессорных вычислительных системах
2005
1963
189
214
Численное исследование и оптимизация трансзвукового обтекания профиля крыла с перфорацией : Автореф. дис. на соиск. учен. степ. к.ф.-м.н. : Спец. 01.02.05
1994
2850
436
504
Fatigue investigation of full-scale transport-airplane wings : Summary of constant-amplitude tests through 1953
1954
989
486
390
Theoretical stability derivatives for a symmetrically tapered wing at low supersonic speeds
1965
1224
401
347
Airfoil characteristics in a nonequilibrium ambient stream based on linearized theory
1964
2280
181
154
Choking effects and some Reynolds number effects on the mach number distribution round a two-dimensional aerofoil in the RAE 10-ft x 7-ft high-speed tunnel
1955
2804
249
205
Note on the effect of size and position of end plates on the lift of a rectangular wing in a wind tunnel
1956
1901
150
134
An approximate method for calculating the laminar boundary layer on an infinite swept wing with arbitrary velocity and suction distribution
1960
1825
223
205
Aerodynamic characteristics of a full-scale faninwing model including results in ground effect with nosefan pitch control
1964
1655
245
212
Theoretical and experimental investigation of the effect of tunnel walls on the forces on an oscillating airfoil in two-dimensional subsonic compressible flow
1956
1162
203
226
Use of two-dimensional data in estimating loads on a 45° sweptback wing with slats and partial-span flaps
1953
1590
395
410
Аэродинамика : [yчебник для втузов]. Ч. 1 : Основы теории. Аэродинамика профиля и крыла
1980
2611
459
442
Wind tunnel tests at mach numbers between 0·6 and 1·4 of a 60° swept wing having an aerofoil section designed for subcritical flow at a Mach number of 1·2
1962
1127
477
417
The Calculation of the warp to produce a given load and the pressures due to a given thickness on thin slender wings in supersonic flow
1967
799
320
285
Low-speed wind-tunnel tests on the effects of various leading-edge modifications on the sectional characteristics of a thin wing
1958
2241
303
255
Measurement of lift, pitching moment and hinge moment on a two-dimensional cusped RAE 102 aerofoil
1956
2376
236
197
On the stressing of multi-rib thin wings of low aspect ratio and rectangular plan-form
1958
2387
20
10
An experimental investigation of the effects of deformation on the aerodynamic characteristics of a sweptback wing
1956
962
184
147
Analytical investigation of icing limit for diamond-shaped airfoil in transonic and supersonic flow
1953
2876
160
137
Wind-tunnel flutter tests on a model delta wing under fixed and free root conditions
1955
1919
325
296
The Aerodynamic forces on an oscillating twodimensional wing in accelerated supersonic flight
1962
2674
32
19
The Pressure-Drag due to blunt leading edges on two-dimensional aerofoils, at transonic and low-supersonic speeds
1967
2346
372
308
Experimental investigation of blast loading on an airfoil in Mach 0.7 airflow with initial angleof - attack change of 28°
1965
2954
500
483
A Method of correlating the ground effects on the longitudinal characteristics of slender wings
1971
2367
480
450
Численное исследование нелокальных граничных условий дальнего поля для задачи дозвукового обтекания крыла
2006
1796
392
373
Skin friction and boundary layer measurements on a three-dimensional wing : Avh. ... vid Tekn. högsk. i Stockholm framlägges ..
1977
2468
320
261
Wind-tunnel tests on the effects of an added mass on the flutter of a model delta wing
1962
2296
168
154
Measurements of the direct pitching-moment derivatives for four wing planforms at transonic speeds
1966
2895
278
303
Measurements of zero-lift drag at supersonic speeds for a symmetrical slender wing model with different roughness bands
1964
2580
210
178
Measurements of skin-friction using surface-pilot tubes in free flight at supersonic speed
1964
1968
476
438
A mean camberline singularity method for two-dimensional steady oscillatory aerofoils and control surfaces in inviscid incompressible flow
1978
1191
83
68
Low-speed wind-tunnel tests on a wing section with plain leading and trailing-edge flaps having boundary-layer control by blowing
1970
2587
500
429
Some measurements in the vortex flow generated by a sharp leading edge having 65 degrees sweep
1960
1748
59
44
Прочность конструкций самолётов : учебное пособие : по специальности 24.05.07 "Самолёто- и вертолётостроение", дисциплине "Прочность конструкций самолётов"
2017
2461
312
294
Труды ЦАГИ. Вып. 2726 : Сравнение методов расчета характеристик ламинарно-турбулентного перехода на крыле с профилем LV6
2013
2835
153
138
Boundary-layer drag of bi-convex wing sections with heat transfer at supersonic speeds
1965
1740
210
189
Low-speed wind tunnel tests on a two-dimensional aerofoil with split flap near the ground
1961
1590
488
437
Calculated spanwise lift distributions, influence functions, and influence coefficient for unswept wings in subsonic flow
1955
1999
478
398
Measurements of the boundary layer and wake of two aerofoil sections at high Reynolds numbers and high-subsonic mach numbers
1973
2207
14
2
Расчет поляры однопанельного крыла самолета при дозвуковых скоростях полета : Учеб. пособие по курсу аэродинамики
2002
2652
253
280
Theoretical comparison of the flow over a flat delta wing and a rectangular pyramid
1963
1782
285
242
Правила постройки судов внутреннего плавания : Врем. нормы прочности судов на подводных крыльях : Утв. и введены в действие МРФ 5/XI 1967 г
1968
1022
260
238
Étude méthodique de l'ailetrapézoidale en considération du décrochement : Principes généraux et bases de recherche
1942
1677
326
261
Конструирование и прочность скоростных судов с новыми режимами движения : Сборник статей
1967
1776
145
117
An experimental study of the pressure and heat transfer distribution on a 70° sweep slab delta wing in hypersonic flow
1963
1080
311
263
Calculated derivatives for rectangular wings oscillating in compressible subsonic flow
1958
1001
198
182
Calculations of the effect of blowing from the leading edges of a slender delta wing
1972
1799
191
201
Comparison between theory and experiment for interference pressure field between wing and body at supersonic speeds
1954
2128
442
386
The velocities induced by distributions of infinite kinked source and vortex lines representing wings with sweep and dihedral in incompressible flow
1971
1924
100
86
A method for calculating the subsonic steady-state loading on an airplane with a wing of arbitrary plan form and stiffness
1953
546
477
462
Some simple conical camber shapes to produce low lift-dependent drag on a slender delta wing
1959
2209
237
217
Stress and distortion analysis of a swept box beam having bulkheads perpendicular to the spars
1950
1245
407
351
Heat-transfer distribution on 70° swept slab delta wings at a mach number of 9.86 and angles of attack up to 90°
1964
2620
461
412
Конструирование механизмов навески и привода средств механизации крыла с элементами проектирования : учебное пособие
2011
1661
422
457
On torsional rigidity and torsional vibration of aerodynamically heated wings having a small amount of pretwist
1960
773
285
243
Wind tunnel tests on antisymmetric flutter of a delta wing with rolling body freedom
1956
1085
70
53
Measurements of pitching moment derivatives for a series of rectangular wings at low wind speeds
1956
879
104
86
An investigation of the flow over a half-wing model with 60-5 degree leading edge sweepback at a high subsonic and supersonic speeds
1960
1367
161
143
Similar solutions for the compressible laminar boundary layer with heat transfer and pressure gradient
1956
877
288
251
Experimental determination of effects of frequency and amplitude on the lateral stability derivatives for a delta, a swept, and an unswept wing oscillating in yaw
1958
1447
299
256
The compressible laminar boundary layer with heat transfer and arbitrary pressure gradient
1956
817
237
196
Supersonic wave drag of nonlifting delta wings with linearly varying thickness ratio
1952
2401
255
206
Measurements of the three - dimensional incompressible turbulent boundary layer induced on the surface of a slender delta - wing by the leading - edge vortex
1975
2697
298
283
Обеспечение качества панелей крыла при выполнении соединений на клепальных автоматах : Автореф. дис. на соиск. учен. степ. к.т.Н. : Спец. 05.07.02
2003
700
216
186
Progress report on an experiment on the effect of surface flexibility on the stability of laminar flow
1962
1454
388
372
Продуктивные качества бройлеров с ампутированными в суточном возрасте крыльями : Автореф. дис. на соиск. учен. степ. к.с.-х.н
1991
762
485
447