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Аэродинамические трубы

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An experimental investigation of wind-tunnel wall conditions for interference-free dynamic measurements
1973
Moore A. W., Wight K. C.
2207
187
Calculation of flexible wall shapes and preparation of control tapes for the Bedford 8-ft X 8-ft wind tunnel
1961
Barritt Marjorie M.
1185
160
A gust tunnel facility
1977
Patel M. H., Hancock G. J.
1707
324
The effect of turbulence on static - pressure tubes
1968
Bradshaw Peter, Goodman D. G.
2659
334
Pressure probes selected for three-dimensional flow measurement
1958
Bryer D. W., Walshe D. E., Garner H. C.
1231
443
Statistical study of transition - point fluctuations in supersonic flow
1954
Evvard John C., Tucker Maurice, Burgess Warten C.
2534
222
The thrust of a supersonic conical nozzle with non-isentropic flow
1958
Rowe P. N.
2529
344
Some investigations into the design of wind tunnels with gas turbine jet engine drives
1953
Higgs H. J.
2452
258
Disturbances in test section of T-325 supersonic wind tunnel
1999
Kosinov Aleksandr Dmitrievič, Semenov N V, Ermolaev Ju G
509
455
Theoretical use of variable porosity in slotted tunnels for minimizing wall interference on dynamic measurements
1972
Garner H. C.
995
11
An investigation of two methods of suppressing shock oscillation ahead of conical centre-body intakes
1962
Griggs C. F.
837
15
The use of woollen felt screens as air cleaners for supersonic wind tunnels
1961
Crane J. F. W.
2565
417
A theoretical exploration of the flow about an electric arc transverse to an airstream using potential flow methods
1968
Broadbent E. G.
2296
325
Notes and comments on some particular features of wind-tunnel design following measurements of flow distribution, wall pressures etc. in the N.P.L. 7 ft. (Low turbulence) wind tunnel
1965
Salter C.; Raymer W. G.
1945
371
Exploratory tests on sting interference at a nach number of 6.8
1961
Peckham D. H.
1425
313
On the flow in an isentropic light piston tunnel
1973
Jones T. V., Schultz D. L., Hedley A. D.
1036
6
Численное профилирование сверхзвуковых пространственных каналов : Автореф. дис. на соиск. учен. степ. д-ра физ.-мат. наук : (01.02.05)
1991
Михайлов Игорь Ефимович
2261
307
The centre-line Mach-number distributions and auxiliary-suction requirements for the A.R.A. 9-ft×8-ft transonic wind tunnel
1960
Haines A. B., Jones C. M.
1652
347
The response time of typical transducer - tube configuration for the measurement of pressures in high-speed wind tunnels
1966
Larcombe M. J., Peto J. W.
1673
378
Основные данные иностранных аэродинамических труб и газодинамических установок : По материалам иностр. печати
1968
2469
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
Burbank Paige B., Byrne Robert W.
1234
399
Основные данные иностранных аэродинамических труб и газодинамических установок : По материалам открытой печати : Таблицы
1974
1309
86
Ударные трубы : Сборник переводных статей
1962
613
235
Some experiments with static tubes at transonic speeds in a slotted-wall wind tunnel
1959
Rogers E. W. E.; Hall I. M.
2950
90
Equilibrium real-gas performance charts for a hyper-sonic shock-tube wind-tunnel employing nitrogen
1963
Bernstein L.
2597
315
The Design and construction of the compressor for the 8th by 8ft hioh-speed wind tunnel at R.A.E. Bedford
1958
Cheshire L. J., Evans J. Y., Goodsell W. A., Wolff P. H.
1630
346
Reibungswirkungen beim Rohrwindkanal
1958
Becker E.
2066
280
The Effects of high pressure on the flow in the reflected shock tunnel
1964
Davies L.; Pennelegion L.; Gough P.; Dolman K.
2208
179
Tests on probes designed to measure stagnation pressure directly in a supersonic stream
1974
Mundell A. R. G.
2046
454
The development of a nozzle for absolute airflow measurement by pitot-static traverse
1964
Ascough J. C.
2646
242
A simple flexible supersonic wind tunnel nozzle for the rapid and accurate variation of flow Mach number
1967
Pierce D.
1072
281
Low speed wind tunnel calibration of a new pitotstatic head (Mk. 10) insensitive to incidence
1964
Mabey D. G.
2515
217
Shock speed and running time measurements in the N. P. L. hypersonic shock tunnel
1959
Henshall B. D.
828
389
Течения в газодинамических установках и соплах : Библиогр. список
1969
2695
372
Wake blockage corrections in a closed wind tunnel for one or two wall-mounted models subject to separated flow
1970
Gould R. W. F.
2543
179
The Calibration of a 60° cone to measure mach number, total pressure and flow angles at supersonic speeds
1963
Andrews D. R., Sawyer W. G.
2927
356
Effects of parallel-jet mixing on downstream Mach number and stagnation pressure with application to engine testing in super tunnels
1953
Bernstein Harry
535
161
Some notes on the flow durations occurring in hypersonic shock tubes
1956
Henshall B. D.
1593
225
Some tests in a slotted-wall tunnel with various slot-entry shapes
1958
Chinneck A.; North N. A.
2943
425
Boundary-induced downwash due to lift in a two-dimensional slotted wind tunnel
1959
Katzoff Samuel, Barger Raymond L.
1142
43
Characteristics of turbulence in a boundary layer with zero pressure gradient
1954
Klebanoff P. S.
666
82
A moving-belt rig for ground simulation in low-speed wind tunnels
1967
Butler S. F. J.; Moy B. A.; Pound T. N.
1109
226
Studies of slotted-wall interference using an electrical analogue. P. 1 P. 2, The electrical analogue to steady and oscillating flow in slotted-wall tunnels. Particular examples of slotted-wall tunnel interference in steady flow
1967
Rushton K. R.
2287
177
Calibration of the flow in the working section of the 3ft×3ft tunnel, National aeronautical establishment
1956
Morris D. E.
1799
444
The Toepler schlieren apparatus
1953
Holder Douglas William, North R. J.
892
352
Wall interference in wind tunnels with slotted and porous boundaries at subsonic speeds
1954
Baldwin Barrett Stone (jr jr); Turner John B.; Knechtel Earl D.
1107
342
Factors affecting the performance of the nozzle of a hypersonic shock tube
1956
Henshall B. D., Gadd G. E.
2835
419
The use of multiple diaphragms in shock tubes
1956
Henshall B. D.
2220
385
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
Auchère Daniel
1840
325
Основные данные аэродинамических труб и газодинамических установок США : По материалам иностр. печати
1968
2327
347
Течение и теплообмен в недорасширенных струях воздуха, истекающих из звукового сопла плазмотрона. Эксперимент и численное моделирование
2001
Афонина Н. Е., Васильевский С. А., Громов В. Г.
1811
387
The N.A.C.A. variable-density wind tunnel
1932
Jacobs Eastman Nixon, Abbott Ira H.
2933
64
Ion tracer technique for airspeed measurement at low densities
1954
Kunkel W. B.
862
68
On the flow in a reflected-shock tunnel
1962
Holder Douglas William, Schultz D. L.
1758
374
Исследование нестационарного теплообмена на модели заостренного цилиндра большого удлинения с применением численной обработки результатов эксперимента
1979
Беспалов А.М., Алифанов О.М., Батура Н.И.
618
36
Wall interference at transonic speeds on a hemisphere-cylinder model
1960
Rogers E. W. E.; Hall I. M.
1565
54
Импульсные аэродинамические трубы : Автореф. дис. на соиск. учен. степ. д.т.н
1989
Затолока Владлен Владимирович
852
100
Fundamental data obtained from shock-tube experiments
1961
Ferri Antonio
1270
240
Wind-tunnel testing
1954
Pope Alan
1696
14
The theory of interference effects on dynamic measurements in slotted-wall tunnels at subsonic speeds and comparisons with experiment
1968
Garner H. C., Moore A. W., Wight K. C.
2787
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
Cox S. G., Pallant R. J., Shaw J. M.
579
196
Experimental investigation at a Mach number of 2.41 of average skin-friction coefficients and velocity profiles for laminar and turbulent boundary layers and an assessment of probe effects
1954
O'Donnell Robert M.
1772
426
Theoretical requirements of tunnel experiments for determining stability derivatives in oscillatory longitudinal disturbances
1955
Neumark S.; Thorpe A. W.
2026
128
Исследование течение газа в цилиндрической рабочей части сверхзвуковой аэродинамической трубы при наличии модели
1972
Харитонов В.Т.
800
3
Собрание сочинений. Т. 4 : Аэродинамика
1949
2481
310
The effect of throat contouring on two-dimensional converging-diverging nozzles at static conditions
1980
Mason Mary L., Putnam Lawrence E., Re Richard J.
1073
355
An optical method of measuring flow velocity in an arc-heated wind tunnel
1966
Buckingham D. J.
1237
82
Импульсные трубы в аэродинамических исследованиях
1978
Друкер И.Г., Затолока В.В., Бошенятов Б.В., Королев Анатолий Семенович
1740
327
Aerodynamic and mechanical tests of a model of a variable Mach number nozzle
1963
Jawor Z. M.
1396
229
Экспериментальные исследования возмущений в пограничном слое и ядре потока в сверхзвуковой аэродинамической трубе при числах М-2; 3 и 4
1975
Илизарова Л.И., Пономарева В.С., Троицкий В.В.
564
396
The N.P.L. 59 in.×9 in. buondary-layer tunnel
1966
Bradshaw Peter, Hellens G. E.
1946
126
Bulk compressibility effects in the R.A.R.D.E. № 3 hypersonic gun tunnel
1966
Clayden W. A.
2027
333
An analytical investigation of the effect of the rate of increase of turbulent kinetic energy in the stream direction on the development of turbulent boundary layers in adverse pressure gradients
1953
Rashis Bernard
1386
71
Notes on some simple strain gauge networks commonly used with wind tunnel balances
1959
Anderson J. R.
2110
329
Flow direction measurements in supersonic wind tunnels
1956
Raney D. J.
2269
132
Determination of stagnation temperatures in the R.A.R.D.E. hypersonic gun tunnel from streak camera measurements of flow velocity
1967
Bowman J. E.
2816
326
A note on derivative apparatus for the N.P.L. 9½ inch high speed tunnel
1956
Bratt J. B.
1265
384
Notes on some German high speed aerodynamic and guided missile research
1946
577
371
A wind-tunnel technique for flutter investigations on swept wings with body freedoms
1955
Jordan P. F.
1129
198
Velocità relativa di bolle di gas in tubi orizzontali
1967
Marruci G.
1638
101
The equilibrium piston technique for gun tunnel operation
1962
East R. A.
2969
216
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
Holder D. R., Farley H. C.
778
368
The design and development of a dynamic pressure control system for the NAE № 3 low speed wind tunnel
1964
Nenonen L. K.
2524
324
An experimental investigation of the reflected-shock pressure-time profiles for air, oxygen, nitrogen, argon, carbon dioxide and acetylene
1967
Davies L.; Edwards D. H.
2202
98
The 7 in x 7 in : Hypersonic wind tunnel at R. A. E. Farnborough
1962
Crane J. F. W.; Crabtree L. F.
2911
369
Аэродинамические трубы малых скоростей : учебное пособие
2017
Рябинин Анатолий Николаевич
1146
413
A short time response stagnation temperature probe
1967
East R. A., Perry J. H.
2662
262
On achieving interference-free results from dynamic tests on half-models in tronsonic wind tunnels
1970
Moore A. W., Wight K. C.
724
232
Determination of boundary-layer transition Reynolds number by surface-temperature measurement of a 10° cone in various NACA supersonic wind tunnels
1953
Ross Albert O.
589
127
Экспериментальное исследование турбулентного смешения спутных неизотермических струй при наличии продольного градиента давления : Расчет спутных турбулентных неизотермических течений при наличии продольного градиента давления
1974
Зимонт В.Л., Мальцев А.И.
2888
316
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
Kline Stephen Jay, Shapiro Ascher Herman
1720
241
Основы газовой динамики и их приложение к расчету сверхзвуковых аэродинамических труб
1965
Паничкин Иван Александрович, Ляхов Андрей Борисович
1097
478
The 9x3 in : Induced-flow high-speed wind tunnel at the National physical laboratory
1953
Holder Douglas William, North R. J.
1288
425
Об исследовании влияния границ потока на аэродинамические характеристики моделей при трансзвуковых скоростях
1978
Книвель Я.Я.
1399
185
Velocity measurements in the Langley I-foot (0.305-meter) hypersonic arc tunnel
1966
Duckett Roy J., Sebacher Daniel I.
2623
274
Estimated power reduction by water injection in a nonreturn supersonic wind tunnel
1953
Cooper Morton, Sevier John R.
2903
246
Аэродинамические трубы дозвуковых и сверхзвуковых скоростей : методическое пособие
2004
2442
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
Lawford J. A.
1462
131
Общие сведения об иностранных аэродинамических трубах
1946
Кузнецов Борис Яковлевич
865
331
Ударные трубы для физико-химических исследований
1966
Солоухин Рем Иванович
1557
449
A Digital automatic multiple pressure recorder
1953
Coss Bert A., Daykin D. R., Jaffe Leonard, Sharp Elmer M.
934
264
Some comments on air condensation effects in a hypersonic helium tunnel
1971
Davies L.; Townsend J. E. G.
1290
266
Техника эксперимента в аэродинамических трубах
1955
Пэнкхерст Р.; Холдер Дуглас Вильям
2175
368
High speed tunnels and other research in Germany
1945
1507
167
The imperial college graphite heated hypersonic windtunnel
1972
Harvey J.K., Jeffery R. W., Uppington D. C.
2300
346
Characteristics of high-speed wind tunnels in the United Kingdom relevant to aeroelastic - model tests
1967
Irwin C. A. K.
1868
182
An index of mathematical tables for shock-tube flow
1956
Henshall B. D.
1179
417
Основные результаты экспериментов на ударных трубах : Пер. с англ
1963
1866
156
Tests of humidity effects on flow in a wind tunnel at much numbers between 2.48 and 4
1956
Monaghan R. J.
1233
126
Wind-tunnel tests on the effect of body freedoms on the flutter of a model wing carrying a localised mass
1958
Gaukroger D. R., Chapple E. W.
1079
381
Feasibility study of high-temperature synthetic-air heater for use with a Mach 8 to 9 hypersonic tunnel
1965
Lezberg Erwin A., Zlatarich Steven A., Price Harold G.
2602
400
The use of sound absorbing walls to reduce dynamic interference in wind tunnels
1976
Mabey D. G.
2872
245
Some measurements of shock-wave attenuation in channels of various cross-sections
1963
Bernstein L.
2105
42
Further development of a high-speed wind tunnel of rectangular cross-section
1938
Bailey Alfred, Wood S. A.
534
137
Controls for the N. A. E. supersonic wind tunnel
1963
Jenkins L. A., Tillson L. J., Kelk G. F.
1403
303
Automatic data reduction equipment for wind tunnels
1958
Rowley G. C.
943
389
Characteristics of major active wind tunnels at the langley research center
1965
Schaefer William T. (jr)
1510
84
Аэродинамические трубы больших скоростей : Пер. с англ
1968
Поуп Аллан, Гойн Кеннис Л.
2507
54
X-Ray instrumentation for density measurements in a supersonic flow field
1952
Dimeff John, Hallett Ralph K., Hansen C. Frederick
743
448
The reduction of dynamic interference by sound-absorbing walls in the RAE 3ft wind tunnel
1979
Mabey D. G.
2876
223
Temperature and pressure studies in the reservoir of a reflected-shock hypersonic tunnel
1967
Lapworth K. C., Townsend J. E.
1391
338
Experimental studies in a low destiny gun tunnel stream
1965
Oguchi Hakuro, Honma Hiroki, Funabiki Katsushi
1670
450
The Heating of air by "Dark" discharge
1968
Hesselgreaves J. E., Nonweiler T. R., Foord T. R.
1710
206
Characteristics of environmental test equipment at the Langley research center
1965
Clevenson Sherman A., MacConochie Ian O.
2112
447
Обзорный анализ экспериментальных исследований, выполненных с помощью некоторых типов ударных труб
2013
Котов Михаил Алтаевич, Кузенов Виктор Витальевич
726
165
Some experiments with sonic throats downstream from the working-section of a slotted-wall high-speed tunnel
1957
Chinneck A.; North N. A.
2874
119
Low speed wind tunnel calibration of a Mk. 9A pitot-static head
1956
Nethaway J. E.
1293
315
Note on the time required for the achievement of steady flow past a slender body in a hypersonic shock tunnel
1961
Holder Douglas William, Schultz D. L.
760
50
Nitrogen condensation in the R.A.R.D.E. hypersonic gas tunnel
1967
Bowman J. E.
621
163
Sur quelques problèmes posés par l'expérimentation en soufflerie aérodynamique: 1-re thèse; ... La similitude physique: 2-e thèse: Thèses présentées à ... l'Univ. de Lille pour obtenir le grade de docteur ès sciences physiques / par André Martinot-Lagarde
1958
Martinot-Lagarde André
1962
207
Одномерные математические модели теплофизических процессов в различных типах ударных труб
2013
Кузенов Виктор Витальевич, Котов Михаил Алтаевич
1447
64
Geschwindigkeitskorrekturen in Windkanälen mit geschlossener und offener Meßstrecke bei kompressibler Unterschallströmung
1961
Cremer Hubert, Schmitz Georg
1848
214
A wind-tunnel test technique for measuring the dynamic rotary stability derivatives at subsonic and supersonic speeds
1956
Beam Benjamin H.
1159
274
Tabulated solutions of the equilibrium gas properties behind the incident and reflected normal shockwave in a shock-tube. I II, Nitrogen. Oxygen
1963
Bernstein L.
2554
292
Mach number distributions along the slotted walls of the N.P.L. 20 in × 8 in : Highspeed wind tunnel
1965
Pearcey H. H., Regan J. D.
2283
62
Анализ систем автоматического регулирования многоконтурной гидродинамической установки с существенно распределенными параметрами
1960
Лэнди Д.Д., Фидлер Г.Д.
974
458
A simple method of improving the supersonic velocity distribution in a transonic tunnel having slotted walls
1959
Hall C. N.
1162
215
Численный расчет изэнтропических течений в осесимметрических гиперзвуковых соплах заданной конфигурации при высоких температурах торможения реального газа; Численный расчет течений неравновесно-диссоциирующего воздуха в осесимметричных соплах
1973
Верховский В.П.
2268
440
Performance of multiple-chamber arc heater with four magnetically spun direct-current arcs
1965
Boldman Donald R., Campbell James P., Simon Paul C.
1609
51
Experimental investigation of two-dimensional tunnel-wall interference at high subsonic speeds
1953
Knechtel Earl D.
2142
10
Ударная труба в химической физике высоких температур
1966
Гейдон Альфред Гордон, Герл И.Р.
1061
243
Wind-tunnel testing
1947
Pope Alan
2072
298
The ames 10-by 14-inch supersonic wind tunnel
1954
Eggers Alfred J. (jr); Nothwang George J. (jr)
1469
251
High pressure real gas drivers and tailoring in shock tunnels
1965
Davies L.
2615
233
On the application of certain statistical methods to wind-tunnel testing
1978
McKie J.
1364
120
The asymmetric adjustable supersonic nozzle for wind-tunnel application
1953
Allen Harry Julian
1121
388
Wind-tunnel investigation of a number of total-pressure tubes at high angles of attack supersonic speeds
1951
Gracey William, Coletti Donald E., Russell Walter R.
2663
42
Experiments on the use of suction through perforated strips for maintaining laminar flow: transition and drag measurements
1958
Gregory N.; Walker W. S.
2901
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
Carter E. C., Tucker K. F.
1566
104
Convection of a pattern of vorticity through a shock wave
1953
Ribner Herbert S.
2199
97
Turbulent boundary-layer and skin-friction measurements in axial flow along cylinders at mach numbers between 0.5 and 3.6
1954
Chapman Dean Roden, Kester Robert H.
975
185
A note on the theory of the Stanton tube
1960
Gadd G. E.
1527
392
Экспериментальное исследование изменения характеристик аэродинамической трубы с камерой Эйфеля в процессе запуска
1974
Беспалов А.М., Михальченко А.Г., Серебряков В.Г.
1110
367
Numerical solutions of oscillatory lift interference. P. 1 P. 2, Oscillatory lift interference in low-speed rectangular tunnels with porous-slotted roof and floor. Oscillatory lift interference in subsonic compressible flow
1972
Rushton K. R., Tomlinson Lucy M.
746
201
Analysis of turbulent heat transfer and flow in the entrance regions of smooth passages
1953
Deissler Robert G.
2066
396