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Аэродинамические трубы

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Analysis of turbulent heat transfer and flow in the entrance regions of smooth passages
1953
Deissler Robert G.
2078
0
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.
759
0
Экспериментальное исследование изменения характеристик аэродинамической трубы с камерой Эйфеля в процессе запуска
1974
Беспалов А.М., Михальченко А.Г., Серебряков В.Г.
1117
0
A note on the theory of the Stanton tube
1960
Gadd G. E.
1539
0
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.
994
0
Convection of a pattern of vorticity through a shock wave
1953
Ribner Herbert S.
2209
0
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.
1578
0
Experiments on the use of suction through perforated strips for maintaining laminar flow: transition and drag measurements
1958
Gregory N.; Walker W. S.
2908
0
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.
2679
0
The asymmetric adjustable supersonic nozzle for wind-tunnel application
1953
Allen Harry Julian
1130
0
On the application of certain statistical methods to wind-tunnel testing
1978
McKie J.
1376
0
High pressure real gas drivers and tailoring in shock tunnels
1965
Davies L.
2623
0
The ames 10-by 14-inch supersonic wind tunnel
1954
Eggers Alfred J. (jr); Nothwang George J. (jr)
1480
0
Wind-tunnel testing
1947
Pope Alan
2083
0
Ударная труба в химической физике высоких температур
1966
Гейдон Альфред Гордон, Герл И.Р.
1076
0
Experimental investigation of two-dimensional tunnel-wall interference at high subsonic speeds
1953
Knechtel Earl D.
2149
0
Performance of multiple-chamber arc heater with four magnetically spun direct-current arcs
1965
Boldman Donald R., Campbell James P., Simon Paul C.
1619
0
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.
2273
0
A simple method of improving the supersonic velocity distribution in a transonic tunnel having slotted walls
1959
Hall C. N.
1168
0
Анализ систем автоматического регулирования многоконтурной гидродинамической установки с существенно распределенными параметрами
1960
Лэнди Д.Д., Фидлер Г.Д.
988
0
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.
2294
0
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.
2559
0
A wind-tunnel test technique for measuring the dynamic rotary stability derivatives at subsonic and supersonic speeds
1956
Beam Benjamin H.
1166
0
Geschwindigkeitskorrekturen in Windkanälen mit geschlossener und offener Meßstrecke bei kompressibler Unterschallströmung
1961
Cremer Hubert, Schmitz Georg
1858
0
Одномерные математические модели теплофизических процессов в различных типах ударных труб
2013
Кузенов Виктор Витальевич, Котов Михаил Алтаевич
1461
0
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
1978
0
Nitrogen condensation in the R.A.R.D.E. hypersonic gas tunnel
1967
Bowman J. E.
632
0
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.
771
0
Low speed wind tunnel calibration of a Mk. 9A pitot-static head
1956
Nethaway J. E.
1312
0
Some experiments with sonic throats downstream from the working-section of a slotted-wall high-speed tunnel
1957
Chinneck A.; North N. A.
2887
0
Обзорный анализ экспериментальных исследований, выполненных с помощью некоторых типов ударных труб
2013
Котов Михаил Алтаевич, Кузенов Виктор Витальевич
737
0
Characteristics of environmental test equipment at the Langley research center
1965
Clevenson Sherman A., MacConochie Ian O.
2126
0
The Heating of air by "Dark" discharge
1968
Hesselgreaves J. E., Nonweiler T. R., Foord T. R.
1720
0
Experimental studies in a low destiny gun tunnel stream
1965
Oguchi Hakuro, Honma Hiroki, Funabiki Katsushi
1683
0
Temperature and pressure studies in the reservoir of a reflected-shock hypersonic tunnel
1967
Lapworth K. C., Townsend J. E.
1405
0
The reduction of dynamic interference by sound-absorbing walls in the RAE 3ft wind tunnel
1979
Mabey D. G.
2886
0
X-Ray instrumentation for density measurements in a supersonic flow field
1952
Dimeff John, Hallett Ralph K., Hansen C. Frederick
756
0
Аэродинамические трубы больших скоростей : Пер. с англ
1968
Поуп Аллан, Гойн Кеннис Л.
2535
0
Characteristics of major active wind tunnels at the langley research center
1965
Schaefer William T. (jr)
1526
0
Automatic data reduction equipment for wind tunnels
1958
Rowley G. C.
953
0
Controls for the N. A. E. supersonic wind tunnel
1963
Jenkins L. A., Tillson L. J., Kelk G. F.
1410
0
Further development of a high-speed wind tunnel of rectangular cross-section
1938
Bailey Alfred, Wood S. A.
554
0
Some measurements of shock-wave attenuation in channels of various cross-sections
1963
Bernstein L.
2115
0
The use of sound absorbing walls to reduce dynamic interference in wind tunnels
1976
Mabey D. G.
2883
0
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.
2610
0
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.
1089
0
Tests of humidity effects on flow in a wind tunnel at much numbers between 2.48 and 4
1956
Monaghan R. J.
1248
0
Основные результаты экспериментов на ударных трубах : Пер. с англ
1963
1876
0
An index of mathematical tables for shock-tube flow
1956
Henshall B. D.
1189
0
Characteristics of high-speed wind tunnels in the United Kingdom relevant to aeroelastic - model tests
1967
Irwin C. A. K.
1880
0
The imperial college graphite heated hypersonic windtunnel
1972
Harvey J.K., Jeffery R. W., Uppington D. C.
2314
0
High speed tunnels and other research in Germany
1945
1520
0
Техника эксперимента в аэродинамических трубах
1955
Пэнкхерст Р.; Холдер Дуглас Вильям
2215
0
Some comments on air condensation effects in a hypersonic helium tunnel
1971
Davies L.; Townsend J. E. G.
1311
0
A Digital automatic multiple pressure recorder
1953
Coss Bert A., Daykin D. R., Jaffe Leonard, Sharp Elmer M.
951
0
Ударные трубы для физико-химических исследований
1966
Солоухин Рем Иванович
1572
0
Общие сведения об иностранных аэродинамических трубах
1946
Кузнецов Борис Яковлевич
875
0
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.
1479
0
Аэродинамические трубы дозвуковых и сверхзвуковых скоростей : методическое пособие
2004
2471
0
Estimated power reduction by water injection in a nonreturn supersonic wind tunnel
1953
Cooper Morton, Sevier John R.
2916
0
Velocity measurements in the Langley I-foot (0.305-meter) hypersonic arc tunnel
1966
Duckett Roy J., Sebacher Daniel I.
2635
0
Об исследовании влияния границ потока на аэродинамические характеристики моделей при трансзвуковых скоростях
1978
Книвель Я.Я.
1414
0
The 9x3 in : Induced-flow high-speed wind tunnel at the National physical laboratory
1953
Holder Douglas William, North R. J.
1298
0
Основы газовой динамики и их приложение к расчету сверхзвуковых аэродинамических труб
1965
Паничкин Иван Александрович, Ляхов Андрей Борисович
1117
0
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
1735
0
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.
2900
0
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.
598
0
On achieving interference-free results from dynamic tests on half-models in tronsonic wind tunnels
1970
Moore A. W., Wight K. C.
740
0
A short time response stagnation temperature probe
1967
East R. A., Perry J. H.
2681
0
Аэродинамические трубы малых скоростей : учебное пособие
2017
Рябинин Анатолий Николаевич
1157
0
The 7 in x 7 in : Hypersonic wind tunnel at R. A. E. Farnborough
1962
Crane J. F. W.; Crabtree L. F.
2936
0
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.
2218
0
The design and development of a dynamic pressure control system for the NAE № 3 low speed wind tunnel
1964
Nenonen L. K.
2535
0
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.
790
0
The equilibrium piston technique for gun tunnel operation
1962
East R. A.
2990
0
Velocità relativa di bolle di gas in tubi orizzontali
1967
Marruci G.
1652
0
A wind-tunnel technique for flutter investigations on swept wings with body freedoms
1955
Jordan P. F.
1144
0
Notes on some German high speed aerodynamic and guided missile research
1946
594
0
A note on derivative apparatus for the N.P.L. 9½ inch high speed tunnel
1956
Bratt J. B.
1282
0
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.
2827
0
Flow direction measurements in supersonic wind tunnels
1956
Raney D. J.
2285
0
Notes on some simple strain gauge networks commonly used with wind tunnel balances
1959
Anderson J. R.
2130
0
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
1406
0
Bulk compressibility effects in the R.A.R.D.E. № 3 hypersonic gun tunnel
1966
Clayden W. A.
2041
0
The N.P.L. 59 in.×9 in. buondary-layer tunnel
1966
Bradshaw Peter, Hellens G. E.
1974
0
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.
579
0
Aerodynamic and mechanical tests of a model of a variable Mach number nozzle
1963
Jawor Z. M.
1412
0
Импульсные трубы в аэродинамических исследованиях
1978
Друкер И.Г., Затолока В.В., Бошенятов Б.В., Королев Анатолий Семенович
1752
0
An optical method of measuring flow velocity in an arc-heated wind tunnel
1966
Buckingham D. J.
1256
0
The effect of throat contouring on two-dimensional converging-diverging nozzles at static conditions
1980
Mason Mary L., Putnam Lawrence E., Re Richard J.
1096
0
Собрание сочинений. Т. 4 : Аэродинамика
1949
2498
0
Исследование течение газа в цилиндрической рабочей части сверхзвуковой аэродинамической трубы при наличии модели
1972
Харитонов В.Т.
815
0
Theoretical requirements of tunnel experiments for determining stability derivatives in oscillatory longitudinal disturbances
1955
Neumark S.; Thorpe A. W.
2041
0
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.
1786
0
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.
597
0
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.
2818
0
Wind-tunnel testing
1954
Pope Alan
1706
0
Fundamental data obtained from shock-tube experiments
1961
Ferri Antonio
1279
0
Импульсные аэродинамические трубы : Автореф. дис. на соиск. учен. степ. д.т.н
1989
Затолока Владлен Владимирович
875
0
Wall interference at transonic speeds on a hemisphere-cylinder model
1960
Rogers E. W. E.; Hall I. M.
1586
0
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.
630
0
On the flow in a reflected-shock tunnel
1962
Holder Douglas William, Schultz D. L.
1776
0
Ion tracer technique for airspeed measurement at low densities
1954
Kunkel W. B.
884
0
The N.A.C.A. variable-density wind tunnel
1932
Jacobs Eastman Nixon, Abbott Ira H.
2943
0
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.
1827
0
Основные данные аэродинамических труб и газодинамических установок США : По материалам иностр. печати
1968
2340
0
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
1879
0
The use of multiple diaphragms in shock tubes
1956
Henshall B. D.
2234
0
Factors affecting the performance of the nozzle of a hypersonic shock tube
1956
Henshall B. D., Gadd G. E.
2861
0
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.
1126
0
The Toepler schlieren apparatus
1953
Holder Douglas William, North R. J.
900
0
Calibration of the flow in the working section of the 3ft×3ft tunnel, National aeronautical establishment
1956
Morris D. E.
1811
0
An experimental investigation of wind-tunnel wall conditions for interference-free dynamic measurements
1973
Moore A. W., Wight K. C.
2233
0
Calculation of flexible wall shapes and preparation of control tapes for the Bedford 8-ft X 8-ft wind tunnel
1961
Barritt Marjorie M.
1202
0
A gust tunnel facility
1977
Patel M. H., Hancock G. J.
1718
0
The effect of turbulence on static - pressure tubes
1968
Bradshaw Peter, Goodman D. G.
2673
0
Pressure probes selected for three-dimensional flow measurement
1958
Bryer D. W., Walshe D. E., Garner H. C.
1261
0
Statistical study of transition - point fluctuations in supersonic flow
1954
Evvard John C., Tucker Maurice, Burgess Warten C.
2564
0
The thrust of a supersonic conical nozzle with non-isentropic flow
1958
Rowe P. N.
2548
0
Some investigations into the design of wind tunnels with gas turbine jet engine drives
1953
Higgs H. J.
2473
0
Disturbances in test section of T-325 supersonic wind tunnel
1999
Kosinov Aleksandr Dmitrievič, Semenov N V, Ermolaev Ju G
529
0
Theoretical use of variable porosity in slotted tunnels for minimizing wall interference on dynamic measurements
1972
Garner H. C.
1013
0
An investigation of two methods of suppressing shock oscillation ahead of conical centre-body intakes
1962
Griggs C. F.
867
0
The use of woollen felt screens as air cleaners for supersonic wind tunnels
1961
Crane J. F. W.
2589
0
A theoretical exploration of the flow about an electric arc transverse to an airstream using potential flow methods
1968
Broadbent E. G.
2313
0
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.
1965
0
Exploratory tests on sting interference at a nach number of 6.8
1961
Peckham D. H.
1461
0
On the flow in an isentropic light piston tunnel
1973
Jones T. V., Schultz D. L., Hedley A. D.
1069
0
Численное профилирование сверхзвуковых пространственных каналов : Автореф. дис. на соиск. учен. степ. д-ра физ.-мат. наук : (01.02.05)
1991
Михайлов Игорь Ефимович
2281
0
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.
1671
0
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.
1721
0
Основные данные иностранных аэродинамических труб и газодинамических установок : По материалам иностр. печати
1968
2492
0
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.
1264
0
Основные данные иностранных аэродинамических труб и газодинамических установок : По материалам открытой печати : Таблицы
1974
1327
0
Ударные трубы : Сборник переводных статей
1962
677
0
Some experiments with static tubes at transonic speeds in a slotted-wall wind tunnel
1959
Rogers E. W. E.; Hall I. M.
2984
0
Equilibrium real-gas performance charts for a hyper-sonic shock-tube wind-tunnel employing nitrogen
1963
Bernstein L.
2615
0
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.
1643
0
Reibungswirkungen beim Rohrwindkanal
1958
Becker E.
2079
0
The Effects of high pressure on the flow in the reflected shock tunnel
1964
Davies L.; Pennelegion L.; Gough P.; Dolman K.
2241
0
Tests on probes designed to measure stagnation pressure directly in a supersonic stream
1974
Mundell A. R. G.
2093
0
The development of a nozzle for absolute airflow measurement by pitot-static traverse
1964
Ascough J. C.
2673
0
A simple flexible supersonic wind tunnel nozzle for the rapid and accurate variation of flow Mach number
1967
Pierce D.
1099
0
Low speed wind tunnel calibration of a new pitotstatic head (Mk. 10) insensitive to incidence
1964
Mabey D. G.
2556
0
Shock speed and running time measurements in the N. P. L. hypersonic shock tunnel
1959
Henshall B. D.
870
0
Течения в газодинамических установках и соплах : Библиогр. список
1969
2717
0
Wake blockage corrections in a closed wind tunnel for one or two wall-mounted models subject to separated flow
1970
Gould R. W. F.
2566
0
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.
2953
0
Effects of parallel-jet mixing on downstream Mach number and stagnation pressure with application to engine testing in super tunnels
1953
Bernstein Harry
560
0
Some notes on the flow durations occurring in hypersonic shock tubes
1956
Henshall B. D.
1635
0
Some tests in a slotted-wall tunnel with various slot-entry shapes
1958
Chinneck A.; North N. A.
2975
0
Boundary-induced downwash due to lift in a two-dimensional slotted wind tunnel
1959
Katzoff Samuel, Barger Raymond L.
1177
0
Characteristics of turbulence in a boundary layer with zero pressure gradient
1954
Klebanoff P. S.
770
0
A moving-belt rig for ground simulation in low-speed wind tunnels
1967
Butler S. F. J.; Moy B. A.; Pound T. N.
1166
0
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.
2340
0