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Испытание в аэродинамической трубе

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Aerodynamic study : Force and moment measurements on three delta wings of aspect ratios 0.83, 1.03 and 1.24 in combination with bodies of fineness ratio 13 at a mach number of 4
1966
Andrews D. R.
751
0
Low-speed wind-tunnel measurements of damping in yaw (nψ) on an A. R. 9 jet-flap complete model
1967
Cox A. P., Butler S. F.
1895
0
Preliminary measurements in a shock tunnel of shock angle and undersurface pressure related to a nonweiler wing
1963
Pennelegion L.; Cash R. F.
2594
0
Wind-tunnel techniques for the measurement of oscillatory derivatives
1963
Bratt J. B.
541
0
Wind tunnel measurements at mach numbers up to 2.80 of the effects of gulling on the longitudinal and lateral stability and drag of a cambered, slender ogee wing
1965
Cook T. A.
1204
0
Wind tunnel tests on a 1/12th scale model of the Bristol type 188 research aircraft with rectangular, wedge intakes at mach numbers from 2.0 to 2.7
1965
Cook T. A.
2846
0
Wind tunnel experiments on a model a tandem rotor helicopter
1961
Halliday A. S., Cox D. K.
2828
0
Low-speed wind-tunnel experiments on a series of sharp-edged delta wings
1966
Earnshaw P. B., Lawford J. A.
766
0
Effects of wing dihedral and planform on stability characteristics of a research model at Mach numbers from 1.80 to 4.63
1965
Feryn Maurice O., Campbell James F.
899
0
A comparison of the lateral controllability with flap and plug ailerons on a sweptback-wing model having full-span flaps
1950
Lovell Powell M. (Jr)
1104
0
Low-speed wind-tunnel tests of a sweptback wing model (Buccaneer Mark I) with blowing at the wing leading edge flaps and blowing over the flaps and drooped ailerons
1971
Butler S. F. J.
1498
0
Gust-tunnel investigation of a wing model with semichord line swept back 60°
1950
Pierce Harold B.
2442
0
Low-speed wind-tunnel measurements of the lift, drag and pitching moment of a series of cropped delta wings
1974
Kirby D. A.
1401
0
Application of luminescent pressure sensor technology to propellers = Приложение технологии люминесцентных датчиков давления к пропеллерам
1995
Bykov A
579
0
Flow unsteadiness and model vibration in wind tunnels at subsonic and transonic speeds
1971
Mabey D. G.
2517
0
A note on the estimation of the effect of wind tunnel walls on the forces on slowly oscillating slender wings
1965
Acum W. E. A.
2143
0
Investigation of some wake vortex characteristics of an inclined ogive-cylinder body at Mach number 2
1958
Jorgensen Leland H., Perkins Edward W.
1693
0
Transonic tunnel tests on a 6% thick, warped 55° sweptback-wing model
1965
Haines A. B., Jones J. C.
859
0
n the effect of fan and thrust engine loading on the transition power requirements of a fan wing
1963
Gregory N.
1879
0
Full-scale wind-tunnel tests of a nonarticulated helicopter rotor
1964
McCloud John L. (III); Biggers James C.
1022
0
Wall corrections for wings oscillating in wind tunnels of closed rectangular section
1963
Acum W. E. A.
2920
0
Wind tunnel tests of a wing fitted with a single lifting fan
1967
Gregory N.; Raymer W. G.; Love Edna M.
2460
0
Аэродинамические трубы дозвуковых и сверхзвуковых скоростей : методическое пособие
2004
2471
0
Wind tunnel tests on a nacelle fitted with two lifting fans in tandem
1967
Gregory N.; Love Edna M.
938
0
Wind-tunnel tests on a rectangular, twin-duct, variable-geometry air intake at supersonic speeds
1967
Dobson M. D.
592
0
A Comparison of results in the A. R. A. transonic tunnel on a small and a large model of a slender wing
1962
Bateman T. E. B.; Haines A. B.
1631
0
Wind tunnel tests between M=0.4 and 0.2 on a cambered wing of slender ogee planform
1965
Dobson M. D.
2132
0
On flutter testing in high-speed wind tunnels
1958
Lambourne N. C.
2489
0
Tip-clearance flow and losses for an isolated compressor blade
1963
Lakshminarayana Budugur, Horlock J. H.
1751
0
Note on wind tunnel tests on the design of cabins
1937
Hartley J. H., Curtis W. H.
559
0
Low speed wind tunnel tests on a series of rectangular wings of varying aspect ratio and aerofoil section
1967
Brebner G. G., Wyatt L. A., Gladys Ilott P.
1267
0
Low-speed wind-tunnel tests on a wing-fuselage model with area suction through perforations at the leading-edge flap knee
1970
Butler S. F. J.; Lawford J. A.
1726
0
Low-speed wind-tunnel measurements of the oscillatory lateral aerodynamic derivatives of a BAC 221 model and comparison of results with similar Concorde and HP 115 data
1971
O'Leary C. O.
2278
0
Tests with a variable ramp intake having combined external/internal compression and a design mach number of 2.2; . / By M. C. Neale and P. S. Lamb
1965
Neale M. C., Lamb P. S.
1651
0
An experimental investigation of the flow through inclined circular tubes at a Mach number of 4.0
1966
Roe P. L.
764
0
Some exploratory tests on a two-dimensional blown-cylinder model in the R.A.E. 2ft×1½ft. transonic wind tunnel
1967
Jones A. F., Buckingham W. R.
2139
0
Experimental study of wind-tunnel wall effects and wall corrections for a general-research v/stol tilt-wing model with flap
1965
Grundwald Kalman J.
1739
0
Wind tunnel tests on the flutter of a swept and unswept wing with ailerons
1960
Hall H.; Rein J. A.
1896
0
Low-speed wind tunnel tests on the effects of taper on low aspect-ratio wings at zero incidence
1961
Peckham D. H.
2245
0
Turbulent flow past two-dimensional bases in supersonic streams
1965
Hastings R. C.
2856
0
Исследование аэродинамики автомобиля : монография
2015
Бернацкий Владислав Витольдович, Острецов Александр Владимирович
859
0
Low-speed wind-tunnel tests on a 1/8th scale model of the Handley-Page HP. 115
1967
Engler P. B. E.; Moss G. F.
699
0
Effects of modifications to the leading-edge region on the stalling characteristics of the NACA 63-O12 airfoil section
1950
Kelly John A.
2983
0
Preliminary results of low speed wind tunnel tests on a gothic wing of aspect ratio 1.O
1960
Peckham D. H., Atkinson S. A.
1529
0
Low-speed wind-tunnel tests on a series of cambered ogee wings
1964
Earnshaw P. B.
1394
0
Wind tunnel measurements of the effect of a jet on the time average and unsteady pressure on the base of a bluff afterbody
1967
Rossiter J. E., Kurn A. G.
1278
0
Low-speed wind-tunnel measurements on a thin sharp-edged delta wing with 70° leading-edge sweep, with particular reference to the position of leading-edge-vortex breakdown
1963
Lawford J. A., Beauchamp A. R.
2938
0
Wind tunnel measurements of lift drag and pitching moment of two highly swept (Λ_LE = 87 deg. and 81 deg.) delta wing-body combination models with small tip fins at M = 2∙47
1960
Bateman P. J.
1834
0
Wind-tunnel test of a full-scale, 1.1 pressure ratio, ducted lift-cruise fan
1964
Giulianetti Demo J., Biggers James C., Corsiglia Victor R.
596
0
Wind tunnel tests at supersonic speeds on a model of the Fairey Delta 2
1964
Dobson M. D.
2200
0
A theory of the blockage effects on bluff bodies and stalled wings in a closed wind tunnel
1965
Maskell E. C.
1715
0
Evaluation of selected refractory oxide materials for use in high-temperature pebble-bed wind-tunnel heat exchangers
1964
Buckley John D., Cocke Bennie W.
2159
0
Wind tunnel measurements of the unsteady pressures in and behind a bomb bay (Canberra)
1965
Rossiter J. E., Kurn A. G.
2702
0
Pressure measurements on a cone cylinder-flare configuration at M = 6.85 and incidences up to 30⁰
1963
Peckham D. H.
2226
0
Suppersonic wind-tunnel flutter tests of two rectangular wings
1958
Guyett P. R.
1009
0
Measurements of the direct pitching-moment derivatives for two-dimensional flow at subsonic and supersonic speeds and for a wing of aspect ratio 4 at subsonic speeds
1962
Bratt J. B., Raymer W.G., Townsend J. E.
2804
0
Balance measurements (excluding drag) on a delta wing aircraft at transonic speeds
1967
Shaw M. M.
2434
0
Upwash interference in a rectangular wind tunnel with closed side walls and porous slotted floor and roof
1963
Holder D. R.
2310
0
The effect of end plates on swept wings at low speed
1950
Riebe John M., Watson James M.
2600
0
Wind tunnel tests at M-2.0 on interference effects between in-take flows in a four-engine nacelle
1964
Dobson M. D.
2125
0
Техника и методы аэрофизического эксперимента. Ч. 1 : Аэродинамические трубы и газодинамические установки
2005
2270
0
Development of hypersonic propulsion tunnels using D. C. plasma arc heating
1963
Raezer S. D., Bunt E. A., Olsen H. L.
784
0
Труды ЦАГИ. Вып. 2723 : Техника и методика струйного эксперимента в аэродинамической трубе Т-116 ЦАГИ
2013
Швалев Ю.Г.
1152
0
Wind tunnel measurements of normal force and pitching moment at a Mach number of 2.00 on a 1:30 scale model of blue streak
1964
Huntley E.
1501
0
Low-speed wind-tunnel tests on some slender airbus configurations
1974
Kirby D. A., Hepworth A. G.
1059
0
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
Lawlor E. F.
1156
0
Low-speed wind-tunnel tests on the effects of various leading-edge modifications on the sectional characteristics of a thin wing
1958
Butler S. F. J.
2283
0
Measurements of the direct pitching-moment derivatives for four wing planforms at transonic speeds
1966
Bratt J. B., Raymer W.G., Townsend J. E.
2922
0
Модельный эксперимент в аэродинамических трубах : Учеб. пособие
1998
Радциг Александр Николаевич, Семенчиков Николай Витальевич
2601
0
Low-speed wind-tunnel tests on a wing section with plain leading and trailing-edge flaps having boundary-layer control by blowing
1970
Lawford J. A., Foster D. N.
2621
0
Информационно-измерительные управляющие системы экспериментальной аэродинамики
2015
Блокин-Мечталин Юрий Константинович
564
0
Моделирование условий полета летательных аппаратов при испытаниях в аэродинамических трубах : учебное пособие для студентов высших учебных заведений, обучающихся по специальности 071300 Гидроаэродинамика
2004
Дубов Борис Сергеевич, Радциг Александр Николаевич, Семенчиков Николай Витальевич, Яковлевский Олег Васильевич
604
0
Some measurements in the vortex flow generated by a sharp leading edge having 65 degrees sweep
1960
Lambourne N. C., Bryer D. W.
1779
0
A low-speed wind tunnel investigation of the tail-plane effectiveness of a model representing the airbus type of aircraft
1970
Lovell D. A.
1440
0
Low-speed wind tunnel tests on a two-dimensional aerofoil with split flap near the ground
1961
Bagley J. A.
1620
0
The use of dust deposition as a means of flow visiualisation
1963
Hignett E. T.
2797
0
Wind tunnel tests on a streamlined fan-lift nacelle. P. 1 P. 2, Tests on nacelle alone and with wings or underfins fitted. The effect of forward speed on the lift produced by a lifting fan and its inlet
1967
Hackett J. E.
2065
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