Drag characteristics obtained from several configurations of the modified X-15-2 airplane up to Mach 6.7

Flight-Determined Subsonic Lift and Drag Characteristics of Seven Lifting-Body and Wing-Body Reentry Vehicle Configurations With Truncated Bases

Wang, K. Charles
Saltzman, Edwin J.
Iliff, Kenneth W.

January 1999

This paper examines flight-measured subsonic lift and drag characteristics of seven lifting-body and...

Preliminary flight-determined subsonic lift and drag characteristics of the X-29A forward-swept-wing airplane

Huckabine, Thomas
Hicks, John W.

August 1989

The X-29A subsonic lift and drag characteristics determined, met, or exceeded predictions, particula...

Aerodynamic characteristics of a hypersonic research airplane concept having a 70 deg swept double-delta wing at Mach numbers from 0.80 to 1.20, with summary of data from 0.20 to 6.0

Penland, J. A.
Dillon, J. L.
Hallissy, J. B.

December 1979

The static longitudinal, lateral, and directional stability characteristics of a hypersonic research...

Preliminary Full-Scale Power-Off Drag of the X-15 Airplane for Mach Numbers from 0.7 to 3.1

Saltzman, Edwin J.

December 1960

Drag characteristics have been obtained for the X-15 airplane during unpowered flight. These data re...

Comparison of Full-scale Lift and Drag Characteristics of the X-15 Airplane with Wind-tunnel Results and Theory

Fetterman, D. E., Jr.
Hopkins, E. J.
Saltzman, E. J.

March 1962

Aerodynamic lift and drag characteristics comparison between full scale and wind tunnel model of X-1...

Flight-measured aerodynamic drag of two large external tanks attached to the X-15-2 airplane at Mach numbers of 1.6 to 2.3

Fisher, D. F.

October 1969

Aerodynamic drag of external fuel tanks attached to X-15-2 airplane at Mach numbers of 1.6 to 2.

Aerodynamic characteristics of a 0.0667-scale model of the X-15A-2 research airplane at transonic speeds

Patterson, J. C., Jr.

March 1966

Aerodynamic characteristics of scale model of X-15 research aircraft determined in transonic pressur...

Hypersonic aerodynamic characteristics of two delta wing X-15 airplane configurations

Stone, D. R.
Goldberg, T. J.
Hefner, J. N.

October 1969

Hypersonic aerodynamic characteristics of delta wing x- 15 airplane configuration

Flight Investigation of the Lift and Drag Characteristics of a Swept-Wing, Multijet, Transport-Type Airplane

Tambor, Ronald

September 1960

The lift and drag characteristics of a Boeing KC-135 airplane were determined during maneuvering fli...

Wind-tunnel/flight correlation study of aerodynamic characteristics of a large flexible supersonic cruise airplane (XB-70-1). 3: A comparison between characteristics predicted from wind-tunnel measurements and those measured in flight

Arnaiz, H. H.
Daugherty, J. C.
Peterson, J. B., Jr.

March 1980

A program was undertaken by NASA to evaluate the accuracy of a method for predicting the aerodynamic...

Preliminary Base Pressures Obtained from the X-15 Airplane at Mach Numbers from 1.1 to 3.2

Saltzman, Edwin J.

August 1961

Base pressure measurements have been made on the fuselage, 10 deg.-wedge vertical fin, and side fair...

Flight measurements of stability and control derivatives of the x-15 research airplane to a mach number of 6.02 and an angle of attack of 25 deg

Yancey, R. B.

November 1964

Flight test data on longitudinal, lateral, and directional stability and control derivatives of X-15...

Flow-field investigations on the X-15 airplane and model up to hypersonic speeds

Palitz, M.
Mc Lain, L. J.

September 1968

Flow distribution in flight test and wind tunnel hypersonic flow of X-15 aircraf

Longitudinal aerodynamic characteristics at Mach numbers from 0.50 to 1.19 of a supersonic transport model with a modified M wing

Taylor, R. T.
Ray, E. J.

June 1967

Longitudinal aerodynamic characteristics at Mach numbers 0.50 to 1.19 of supersonic transport model ...

Wind-tunnel investigation of the flow field beneath the fuselage of the X-15 airplane at Mach numbers from 4 to 8

Palitz, M.
Montoya, E. J.

November 1967

Wind tunnel study of flow field beneath X-15 aircraft fuselage at supersonic to hypersonic speed

Flight-Determined Subsonic Lift and Drag Characteristics of Seven Lifting-Body and Wing-Body Reentry Vehicle Configurations With Truncated Bases

Wang, K. Charles
Saltzman, Edwin J.
Iliff, Kenneth W.

January 1999

This paper examines flight-measured subsonic lift and drag characteristics of seven lifting-body and...

Preliminary flight-determined subsonic lift and drag characteristics of the X-29A forward-swept-wing airplane

Huckabine, Thomas
Hicks, John W.

August 1989

The X-29A subsonic lift and drag characteristics determined, met, or exceeded predictions, particula...

Aerodynamic characteristics of a hypersonic research airplane concept having a 70 deg swept double-delta wing at Mach numbers from 0.80 to 1.20, with summary of data from 0.20 to 6.0

Penland, J. A.
Dillon, J. L.
Hallissy, J. B.

December 1979

The static longitudinal, lateral, and directional stability characteristics of a hypersonic research...

Preliminary Full-Scale Power-Off Drag of the X-15 Airplane for Mach Numbers from 0.7 to 3.1

Saltzman, Edwin J.

December 1960

Drag characteristics have been obtained for the X-15 airplane during unpowered flight. These data re...

Comparison of Full-scale Lift and Drag Characteristics of the X-15 Airplane with Wind-tunnel Results and Theory

Fetterman, D. E., Jr.
Hopkins, E. J.
Saltzman, E. J.

March 1962

Aerodynamic lift and drag characteristics comparison between full scale and wind tunnel model of X-1...

Flight-measured aerodynamic drag of two large external tanks attached to the X-15-2 airplane at Mach numbers of 1.6 to 2.3

Fisher, D. F.

October 1969

Aerodynamic drag of external fuel tanks attached to X-15-2 airplane at Mach numbers of 1.6 to 2.

Aerodynamic characteristics of a 0.0667-scale model of the X-15A-2 research airplane at transonic speeds

Patterson, J. C., Jr.

March 1966

Aerodynamic characteristics of scale model of X-15 research aircraft determined in transonic pressur...

Hypersonic aerodynamic characteristics of two delta wing X-15 airplane configurations

Stone, D. R.
Goldberg, T. J.
Hefner, J. N.

October 1969

Hypersonic aerodynamic characteristics of delta wing x- 15 airplane configuration

Flight Investigation of the Lift and Drag Characteristics of a Swept-Wing, Multijet, Transport-Type Airplane

Tambor, Ronald

September 1960

The lift and drag characteristics of a Boeing KC-135 airplane were determined during maneuvering fli...

Wind-tunnel/flight correlation study of aerodynamic characteristics of a large flexible supersonic cruise airplane (XB-70-1). 3: A comparison between characteristics predicted from wind-tunnel measurements and those measured in flight

Arnaiz, H. H.
Daugherty, J. C.
Peterson, J. B., Jr.

March 1980

A program was undertaken by NASA to evaluate the accuracy of a method for predicting the aerodynamic...

Preliminary Base Pressures Obtained from the X-15 Airplane at Mach Numbers from 1.1 to 3.2

Saltzman, Edwin J.

August 1961

Base pressure measurements have been made on the fuselage, 10 deg.-wedge vertical fin, and side fair...

Flight measurements of stability and control derivatives of the x-15 research airplane to a mach number of 6.02 and an angle of attack of 25 deg

Yancey, R. B.

November 1964

Flight test data on longitudinal, lateral, and directional stability and control derivatives of X-15...

Flow-field investigations on the X-15 airplane and model up to hypersonic speeds

Palitz, M.
Mc Lain, L. J.

September 1968

Flow distribution in flight test and wind tunnel hypersonic flow of X-15 aircraf

Longitudinal aerodynamic characteristics at Mach numbers from 0.50 to 1.19 of a supersonic transport model with a modified M wing

Taylor, R. T.
Ray, E. J.

June 1967

Longitudinal aerodynamic characteristics at Mach numbers 0.50 to 1.19 of supersonic transport model ...

Wind-tunnel investigation of the flow field beneath the fuselage of the X-15 airplane at Mach numbers from 4 to 8

Palitz, M.
Montoya, E. J.

November 1967

Wind tunnel study of flow field beneath X-15 aircraft fuselage at supersonic to hypersonic speed

Flight-Determined Subsonic Lift and Drag Characteristics of Seven Lifting-Body and Wing-Body Reentry Vehicle Configurations With Truncated Bases

Wang, K. Charles
Saltzman, Edwin J.
Iliff, Kenneth W.

January 1999

This paper examines flight-measured subsonic lift and drag characteristics of seven lifting-body and...

Preliminary flight-determined subsonic lift and drag characteristics of the X-29A forward-swept-wing airplane

Huckabine, Thomas
Hicks, John W.

August 1989

The X-29A subsonic lift and drag characteristics determined, met, or exceeded predictions, particula...

Aerodynamic characteristics of a hypersonic research airplane concept having a 70 deg swept double-delta wing at Mach numbers from 0.80 to 1.20, with summary of data from 0.20 to 6.0

Penland, J. A.
Dillon, J. L.
Hallissy, J. B.

December 1979

The static longitudinal, lateral, and directional stability characteristics of a hypersonic research...

Drag characteristics obtained from several configurations of the modified X-15-2 airplane up to Mach 6.7

Abstract

Extracted data

Drag characteristics obtained from several configurations of the modified X-15-2 airplane up to Mach 6.7

Abstract

Extracted data

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