Large-scale low-speed wind-tunnel tests of a delta winged supersonic transport model to determine aerodynamic effects of forward or reverse thrust

Low-speed wind tunnel tests of 1/9-scale model of a variable-sweep supersonic cruise aircraft

Mclemore, H. C.
Sewall, W. G.
Parlett, L. P.

June 1977

Tests were conducted in the Langley full-scale tunnel to determine the aerodynamic characteristics a...

Analytical Investigation of the Reentry Behavior of the ''flying Wind Tunnel'' Test Vehicle, with Some Effects of Threshold and Torque Level of a Roll-rate Control System

Jaquet, B. M.
Fletcher, H. S.

July 1962

Analytical investigation of reentry behavior of flying wind tunnel test vehicle with some effects of...

Effects of upper-surface blowing and thrust vectoring on low-speed aerodynamic characteristics of a large-scale supersonic transport model

Shivers, J. P.
Mclemore, H. C.
Coe, P. L., Jr.

November 1975

Tests were conducted in the Langley full-scale tunnel to determine the low-speed aerodynamic charact...

Large-scale wind-tunnel investigation of the low-speed aerodynamic characteristics of a supersonic transport model having variable- sweep wings

Cook, A. M.
Aoyagi, K.
Greif, R. K.

May 1965

Large scale wind tunnel investigation of low speed aerodynamic characteristics of supersonic transpo...

Effects of upper-surface blowing and thrust vectoring on low speed aerodynamic characteristics of a large-scale supersonic transport model

Mclemore, H. C.
Shivers, J. P.
Coe, P. L., Jr.

November 1976

Tests were conducted in a full scale tunnel to determine the low speed aerodynamic characteristics o...

Low speed wind tunnel tests of 1/10-scale model of a blended-arrow supersonic cruise aircraft

Parlett, L. P.
Mclemore, H. C.

June 1977

Low speed static force tests have been conducted in a full scale tunnel to determine the low speed a...

Wind-tunnel investigation of the thrust augmentor performance of a large-scale swept wing model

Koenig, D. G.
Falarski, M. D.

February 1979

Tests were made in the Ames 40- by 80-foot wind tunnel to determine the forward speed effects on win...

Aerodynamic characteristics of a hypersonic research airplane concept having a 70 deg swept double-delta wing at Mach number 0.2

Dillon, J. L.
Penland, J. A.
Creel, T. R., Jr.

September 1978

A wind-tunnel of the static longitudinal, lateral and directional stability characteristics of a hyp...

Large-scale wind tunnel tests of a subsonic transport with AFT engine nacelles and high tail

Aoyagi, K.
Tolhurst, W. H., Jr.

January 1967

Static longitudinal stability and control at angles of attack above those for wing stall in large-sc...

Low-speed wind-tunnel investigation of a large-scale advanced arrow wing supersonic transport configuration with engines mounted above the wing for upper-surface blowing

Mclemore, H. C.
Coe, P. L., Jr.
Shivers, J. P.

August 1975

The Langley full scale tunnel was used to investigate the low speed stability and control of an adva...

Wing planform effects at supersonic speeds for an advanced fighter configuration

Miller, D. S.
Wood, R. M.

March 1984

Four advanced fighter configurations, which differed in wing planform and airfoil shape, were invest...

Low-speed wind-tunnel investigation of a large scale advanced arrow-wing supersonic transport configuration with engines mounted above wing for upper-surface blowing

Coe, P. L., Jr.
Mclemore, H. C.
Shivers, J. P.

December 1976

Tests have been conducted in a full scale tunnel to determine the low speed aerodynamic characterist...

Wind tunnel investigation of the low speed high lift aerodynamics of a one-fifth scale variable sweep supersonic transport

Cook, A. M.

October 1968

Wind tunnel tests to determine low speed high lift aerodynamics of one-fifth scale variable sweep su...

Large scale wind tunnel investigation to improve the low speed longitudinal stability at high lift of a supersonic transport with variable-sweep wings

Cook, A. M.
Jones, D. G.

January 1969

Large scale wind tunnel tests to improve longitudinal stability of supersonic transports with variab...

Effect of a simulated engine jet blowing above an arrow wing at Mach 2.0

Hayes, C.
Shrout, B. L.

January 1977

The effects of a gas jet simulating a turbojet engine exhaust blowing above a cambered and twisted a...

Low-speed wind tunnel tests of 1/9-scale model of a variable-sweep supersonic cruise aircraft

Mclemore, H. C.
Sewall, W. G.
Parlett, L. P.

June 1977

Tests were conducted in the Langley full-scale tunnel to determine the aerodynamic characteristics a...

Analytical Investigation of the Reentry Behavior of the ''flying Wind Tunnel'' Test Vehicle, with Some Effects of Threshold and Torque Level of a Roll-rate Control System

Jaquet, B. M.
Fletcher, H. S.

July 1962

Analytical investigation of reentry behavior of flying wind tunnel test vehicle with some effects of...

Effects of upper-surface blowing and thrust vectoring on low-speed aerodynamic characteristics of a large-scale supersonic transport model

Shivers, J. P.
Mclemore, H. C.
Coe, P. L., Jr.

November 1975

Tests were conducted in the Langley full-scale tunnel to determine the low-speed aerodynamic charact...

Large-scale wind-tunnel investigation of the low-speed aerodynamic characteristics of a supersonic transport model having variable- sweep wings

Cook, A. M.
Aoyagi, K.
Greif, R. K.

May 1965

Large scale wind tunnel investigation of low speed aerodynamic characteristics of supersonic transpo...

Effects of upper-surface blowing and thrust vectoring on low speed aerodynamic characteristics of a large-scale supersonic transport model

Mclemore, H. C.
Shivers, J. P.
Coe, P. L., Jr.

November 1976

Tests were conducted in a full scale tunnel to determine the low speed aerodynamic characteristics o...

Low speed wind tunnel tests of 1/10-scale model of a blended-arrow supersonic cruise aircraft

Parlett, L. P.
Mclemore, H. C.

June 1977

Low speed static force tests have been conducted in a full scale tunnel to determine the low speed a...

Wind-tunnel investigation of the thrust augmentor performance of a large-scale swept wing model

Koenig, D. G.
Falarski, M. D.

February 1979

Tests were made in the Ames 40- by 80-foot wind tunnel to determine the forward speed effects on win...

Aerodynamic characteristics of a hypersonic research airplane concept having a 70 deg swept double-delta wing at Mach number 0.2

Dillon, J. L.
Penland, J. A.
Creel, T. R., Jr.

September 1978

A wind-tunnel of the static longitudinal, lateral and directional stability characteristics of a hyp...

Large-scale wind tunnel tests of a subsonic transport with AFT engine nacelles and high tail

Aoyagi, K.
Tolhurst, W. H., Jr.

January 1967

Static longitudinal stability and control at angles of attack above those for wing stall in large-sc...

Low-speed wind-tunnel investigation of a large-scale advanced arrow wing supersonic transport configuration with engines mounted above the wing for upper-surface blowing

Mclemore, H. C.
Coe, P. L., Jr.
Shivers, J. P.

August 1975

The Langley full scale tunnel was used to investigate the low speed stability and control of an adva...

Wing planform effects at supersonic speeds for an advanced fighter configuration

Miller, D. S.
Wood, R. M.

March 1984

Four advanced fighter configurations, which differed in wing planform and airfoil shape, were invest...

Low-speed wind-tunnel investigation of a large scale advanced arrow-wing supersonic transport configuration with engines mounted above wing for upper-surface blowing

Coe, P. L., Jr.
Mclemore, H. C.
Shivers, J. P.

December 1976

Tests have been conducted in a full scale tunnel to determine the low speed aerodynamic characterist...

Wind tunnel investigation of the low speed high lift aerodynamics of a one-fifth scale variable sweep supersonic transport

Cook, A. M.

October 1968

Wind tunnel tests to determine low speed high lift aerodynamics of one-fifth scale variable sweep su...

Large scale wind tunnel investigation to improve the low speed longitudinal stability at high lift of a supersonic transport with variable-sweep wings

Cook, A. M.
Jones, D. G.

January 1969

Large scale wind tunnel tests to improve longitudinal stability of supersonic transports with variab...

Effect of a simulated engine jet blowing above an arrow wing at Mach 2.0

Hayes, C.
Shrout, B. L.

January 1977

The effects of a gas jet simulating a turbojet engine exhaust blowing above a cambered and twisted a...

Low-speed wind tunnel tests of 1/9-scale model of a variable-sweep supersonic cruise aircraft

Mclemore, H. C.
Sewall, W. G.
Parlett, L. P.

June 1977

Tests were conducted in the Langley full-scale tunnel to determine the aerodynamic characteristics a...

Analytical Investigation of the Reentry Behavior of the ''flying Wind Tunnel'' Test Vehicle, with Some Effects of Threshold and Torque Level of a Roll-rate Control System

Jaquet, B. M.
Fletcher, H. S.

July 1962

Analytical investigation of reentry behavior of flying wind tunnel test vehicle with some effects of...

Effects of upper-surface blowing and thrust vectoring on low-speed aerodynamic characteristics of a large-scale supersonic transport model

Shivers, J. P.
Mclemore, H. C.
Coe, P. L., Jr.

November 1975

Tests were conducted in the Langley full-scale tunnel to determine the low-speed aerodynamic charact...

Large-scale low-speed wind-tunnel tests of a delta winged supersonic transport model to determine aerodynamic effects of forward or reverse thrust

Abstract

Extracted data

Large-scale low-speed wind-tunnel tests of a delta winged supersonic transport model to determine aerodynamic effects of forward or reverse thrust

Abstract

Extracted data

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