Аэродинамические трубы
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An experimental investigation of wind-tunnel wall conditions for interference-free dynamic measurements
1973
2207
205
187
Calculation of flexible wall shapes and preparation of control tapes for the Bedford 8-ft X 8-ft wind tunnel
1961
1185
197
160
Some investigations into the design of wind tunnels with gas turbine jet engine drives
1953
2452
220
258
Theoretical use of variable porosity in slotted tunnels for minimizing wall interference on dynamic measurements
1972
995
19
11
An investigation of two methods of suppressing shock oscillation ahead of conical centre-body intakes
1962
837
24
15
A theoretical exploration of the flow about an electric arc transverse to an airstream using potential flow methods
1968
2296
387
325
Численное профилирование сверхзвуковых пространственных каналов : Автореф. дис. на соиск. учен. степ. д-ра физ.-мат. наук : (01.02.05)
1991
2261
379
307
The centre-line Mach-number distributions and auxiliary-suction requirements for the A.R.A. 9-ft×8-ft transonic wind tunnel
1960
1652
429
347
The response time of typical transducer - tube configuration for the measurement of pressures in high-speed wind tunnels
1966
1673
427
378
Основные данные иностранных аэродинамических труб и газодинамических установок : По материалам иностр. печати
1968
2469
419
379
The aerodynamic design and calibration of an asymmetric variable Mach number nozzle with a sliding block for the Mach number range 1.27 to 2.75
1953
1234
418
399
Основные данные иностранных аэродинамических труб и газодинамических установок : По материалам открытой печати : Таблицы
1974
1309
102
86
Some experiments with static tubes at transonic speeds in a slotted-wall wind tunnel
1959
2950
112
90
Equilibrium real-gas performance charts for a hyper-sonic shock-tube wind-tunnel employing nitrogen
1963
2597
349
315
The Design and construction of the compressor for the 8th by 8ft hioh-speed wind tunnel at R.A.E. Bedford
1958
1630
332
346
Tests on probes designed to measure stagnation pressure directly in a supersonic stream
1974
2046
500
454
The development of a nozzle for absolute airflow measurement by pitot-static traverse
1964
2646
258
242
A simple flexible supersonic wind tunnel nozzle for the rapid and accurate variation of flow Mach number
1967
1072
315
281
Low speed wind tunnel calibration of a new pitotstatic head (Mk. 10) insensitive to incidence
1964
2515
274
217
Wake blockage corrections in a closed wind tunnel for one or two wall-mounted models subject to separated flow
1970
2543
204
179
The Calibration of a 60° cone to measure mach number, total pressure and flow angles at supersonic speeds
1963
2927
415
356
Effects of parallel-jet mixing on downstream Mach number and stagnation pressure with application to engine testing in super tunnels
1953
535
179
161
Calibration of the flow in the working section of the 3ft×3ft tunnel, National aeronautical establishment
1956
1799
483
444
Wall interference in wind tunnels with slotted and porous boundaries at subsonic speeds
1954
1107
402
342
Contribution à l'étude expérimentale d'un compresseur à piston libre : 1-re thèse prés. ... à la Fac. des sciences de l'Univ. de Grenoble ..
1969
1840
368
325
Основные данные аэродинамических труб и газодинамических установок США : По материалам иностр. печати
1968
2327
394
347
Течение и теплообмен в недорасширенных струях воздуха, истекающих из звукового сопла плазмотрона. Эксперимент и численное моделирование
2001
1811
485
387
The theory of interference effects on dynamic measurements in slotted-wall tunnels at subsonic speeds and comparisons with experiment
1968
2787
220
184
The Pressure calibration of the R. A. E. 6 inch diameter shock tube with a view to its use as the driver of a cold high-density hypersonic tunnel
1963
579
233
196
Theoretical requirements of tunnel experiments for determining stability derivatives in oscillatory longitudinal disturbances
1955
2026
144
128
Исследование течение газа в цилиндрической рабочей части сверхзвуковой аэродинамической трубы при наличии модели
1972
800
17
3
The effect of throat contouring on two-dimensional converging-diverging nozzles at static conditions
1980
1073
384
355
Экспериментальные исследования возмущений в пограничном слое и ядре потока в сверхзвуковой аэродинамической трубе при числах М-2; 3 и 4
1975
564
462
396
Notes on some simple strain gauge networks commonly used with wind tunnel balances
1959
2110
359
329
Determination of stagnation temperatures in the R.A.R.D.E. hypersonic gun tunnel from streak camera measurements of flow velocity
1967
2816
398
326
A wind-tunnel technique for flutter investigations on swept wings with body freedoms
1955
1129
220
198
Problems associated with the use of a false wall as a reflection for half model tests in the de Havilland High Speed Wind Tunnel
1962
778
386
368
The design and development of a dynamic pressure control system for the NAE № 3 low speed wind tunnel
1964
2524
351
324
An experimental investigation of the reflected-shock pressure-time profiles for air, oxygen, nitrogen, argon, carbon dioxide and acetylene
1967
2202
113
98
On achieving interference-free results from dynamic tests on half-models in tronsonic wind tunnels
1970
724
279
232
Determination of boundary-layer transition Reynolds number by surface-temperature measurement of a 10° cone in various NACA supersonic wind tunnels
1953
589
150
127
Experimental investigation of the effects of cooling on friction and on boundarylayer translation for low-speed gas flow at the entry of a tube
1953
1720
291
241
Основы газовой динамики и их приложение к расчету сверхзвуковых аэродинамических труб
1965
1097
458
478
The 9x3 in : Induced-flow high-speed wind tunnel at the National physical laboratory
1953
1288
482
425
Об исследовании влияния границ потока на аэродинамические характеристики моделей при трансзвуковых скоростях
1978
1399
208
185
Estimated power reduction by water injection in a nonreturn supersonic wind tunnel
1953
2903
284
246
Аэродинамические трубы дозвуковых и сверхзвуковых скоростей : методическое пособие
2004
2442
388
339
Measurements of velocity fluctuations in the working section of the R. A. E. 4ft.×3ft. wind tunnel with flow disturbances in the second diffuser
1959
1462
152
131
Characteristics of high-speed wind tunnels in the United Kingdom relevant to aeroelastic - model tests
1967
1868
215
182
Tests of humidity effects on flow in a wind tunnel at much numbers between 2.48 and 4
1956
1233
144
126
Wind-tunnel tests on the effect of body freedoms on the flutter of a model wing carrying a localised mass
1958
1079
455
381
Feasibility study of high-temperature synthetic-air heater for use with a Mach 8 to 9 hypersonic tunnel
1965
2602
501
400
The reduction of dynamic interference by sound-absorbing walls in the RAE 3ft wind tunnel
1979
2876
239
223
Temperature and pressure studies in the reservoir of a reflected-shock hypersonic tunnel
1967
1391
393
338
Обзорный анализ экспериментальных исследований, выполненных с помощью некоторых типов ударных труб
2013
726
200
165
Some experiments with sonic throats downstream from the working-section of a slotted-wall high-speed tunnel
1957
2874
107
119
Note on the time required for the achievement of steady flow past a slender body in a hypersonic shock tunnel
1961
760
64
50
Одномерные математические модели теплофизических процессов в различных типах ударных труб
2013
1447
79
64
Geschwindigkeitskorrekturen in Windkanälen mit geschlossener und offener Meßstrecke bei kompressibler Unterschallströmung
1961
1848
270
214
A wind-tunnel test technique for measuring the dynamic rotary stability derivatives at subsonic and supersonic speeds
1956
1159
303
274
Tabulated solutions of the equilibrium gas properties behind the incident and reflected normal shockwave in a shock-tube. I II, Nitrogen. Oxygen
1963
2554
338
292
Mach number distributions along the slotted walls of the N.P.L. 20 in × 8 in : Highspeed wind tunnel
1965
2283
79
62
Анализ систем автоматического регулирования многоконтурной гидродинамической установки с существенно распределенными параметрами
1960
974
477
458
A simple method of improving the supersonic velocity distribution in a transonic tunnel having slotted walls
1959
1162
245
215
Performance of multiple-chamber arc heater with four magnetically spun direct-current arcs
1965
1609
66
51
Experimental investigation of two-dimensional tunnel-wall interference at high subsonic speeds
1953
2142
23
10
Wind-tunnel investigation of a number of total-pressure tubes at high angles of attack supersonic speeds
1951
2663
55
42
Experiments on the use of suction through perforated strips for maintaining laminar flow: transition and drag measurements
1958
2901
173
157
Some results of an investigation into the use of air injection in a model of the diffuser for the A. R. A. supersonic tunnel
1958
1566
120
104
Turbulent boundary-layer and skin-friction measurements in axial flow along cylinders at mach numbers between 0.5 and 3.6
1954
975
198
185