Investigation of the loading characteristics of the lifting surfaces and the speed brakes of a 0.067-scale model of the north american x-15 airplane (configuration 3) at Mach numbers of 2.29, 2.98, and 4.65 /

Full-scale wind-tunnel investigation of the aerodynamic characteristics of the X-24A lifting body aircraft /

Mort, Kenneth W.
Falarski, Michael D.
U.S. Army Aeronautical Research Laboratory.
Ames Research Center.
United States. National Aeronautics and Space Administration.

"August 1970."Cover title.Includes bibliographical references (p. 6).Mode of access: Internet

Aerodynamic-derivative characteristics of the X-15 research airplane as determined from flight tests for mach numbers from 0.6 to 3.4 /

Yancey, Roxanah B.
United States. National Aeronautics and Space Administration.

Cover title."January 1962."Aerodynamics, aircraft; Aerodynamics, missiles and space vehicles; Aircra...

Static stability and control characteristics of an airplane model with tail surfaces outboard of the wing tips at a mach number of 2.01 /

Driver, Cornelius.
Spearman, M. Leroy.
United States. National Aeronautics and Space Administration.

"September 1959."Cover title.Includes bibliographical references (p. 8).Mode of access: Internet

Investigation of the aerodynamic characteristics of a 0.067-scale model of the x-15 airplane (configuration 3) at mach numbers of 2.29, 2.98, and 4.65 /

Franklin, Arthur E.
Lust, Robert M.
Langley Research Center.

January 1959

"November 1959."Cover title.Includes bibliographical references (p. 9).Mode of access: Internet

Investigation of the subsonic stability and control characteristics of a 1/7-scale model of the North American X-15 airplane with and without fuselage forebody strakes /

Hassell, James L.
Hewes, Donald E.
United States. National Aeronautics and Space Administration.

"February 1960."Cover title.Includes bibliographical references (p. 17).Mode of access: Internet

Pressure distribution of a 0.0667-scale model of the X-15 airplane for an angle-of-attack range of 0° to 28° at mach numbers of 2.30, 288, and 4.65 /

Hodge, B. Leon.
Burbank, Paige B.
United States. National Aeronautics and Space Administration.

"May 1960."Cover title.Includes bibliographical references (p. 8).Mode of access: Internet

Stability and control characteristics of a 0.0667-scale model of the final version of the North American X-15 research airplane (configuration 3) at transonic speeds /

Osborne, Robert S.
Ware, George M.
United States. National Aeronautics and Space Administration.

"April 1963."Cover title.Includes bibliographical references (p. 8).Mode of access: Internet

Aerodynamic and landing measurements obtained during the first powered flight of the North American X-15 research airplane /

United States. National Aeronautics and Space Administration.
Flight Research Center (U.S.)

"January 1960."Cover title.Includes bibliographical references (p. 17).Mode of access: Internet

Basic pressure measurements on a 0.0667-scale model of the North American X-15 research airplane at transonic speeds /

Osborne, Robert S.
Stafford, Virginia C.
Langley Research Center.
United States. National Aeronautics and Space Administration.

"Langley Research Center, Langely Field, Va.""October 1960."Cover title.Includes bibliographical ref...

Preliminary base pressures obtained from the X-15 airplane at mach numbers from 1.1 to 3.2 /

Saltzman, Edwin J.
United States. National Aeronautics and Space Administration.

Cover title."August 1961."Aerodynamics, aircraft;Aerodynamics, missiles and space vehicles; Vehicle ...

Launch, low-speed, and landing characteristics determined from the first flight of the North American X-15 research airplane /

Finch, Thomas W.
Matranga, Gene J.
United States. National Aeronautics and Space Administration.

"September 1959."Cover title.Includes bibliographical references (p. 11).Mode of access: Internet

Static longitudinal, directional, and lateral stability and control data at a mach number of 6.83 of the final configuration of the X-15 research airplane /

Penland, Jim A.
Fetterman, Jr., David E.
Langley Research Center.

January 1960

"April 1960"--Cover.Caption title.Includes bibliographical references (p. 10-11).Mode of access: Int...

Landing loads and dynamics of the X-15 airplane /

McKay, James M..
Kordes, Eldon E.
Flight Research Center.

January 1962

"March 1962."Includes bibliographical references (p. 11).Mode of access: Internet

Low-speed measurements of oscillatory lateral stability derivatives of a 1/7-scale model of the North American X-15 airplane /

Paulson, John W.
Hassell, James L.
United States. National Aeronautics and Space Administration.

"November 1959."Cover title.Includes bibliographical references (p. 6).Mode of access: Internet

Aerodynamic loads at mach numbers from 0.70 to 2.22 on an airplane model having a wing and canard of triangular plan form and either single or twin vertical tails /

Peterson, Victor L.
Menees, Gene P.
United States. National Aeronautics and Space Administration.

Cover title."June 1961."Aerodynamics, aircraft; Stresses and loads.Includes bibliographical referenc...

Full-scale wind-tunnel investigation of the aerodynamic characteristics of the X-24A lifting body aircraft /

Mort, Kenneth W.
Falarski, Michael D.
U.S. Army Aeronautical Research Laboratory.
Ames Research Center.
United States. National Aeronautics and Space Administration.

"August 1970."Cover title.Includes bibliographical references (p. 6).Mode of access: Internet

Aerodynamic-derivative characteristics of the X-15 research airplane as determined from flight tests for mach numbers from 0.6 to 3.4 /

Yancey, Roxanah B.
United States. National Aeronautics and Space Administration.

Cover title."January 1962."Aerodynamics, aircraft; Aerodynamics, missiles and space vehicles; Aircra...

Static stability and control characteristics of an airplane model with tail surfaces outboard of the wing tips at a mach number of 2.01 /

Driver, Cornelius.
Spearman, M. Leroy.
United States. National Aeronautics and Space Administration.

"September 1959."Cover title.Includes bibliographical references (p. 8).Mode of access: Internet

Investigation of the aerodynamic characteristics of a 0.067-scale model of the x-15 airplane (configuration 3) at mach numbers of 2.29, 2.98, and 4.65 /

Franklin, Arthur E.
Lust, Robert M.
Langley Research Center.

January 1959

"November 1959."Cover title.Includes bibliographical references (p. 9).Mode of access: Internet

Investigation of the subsonic stability and control characteristics of a 1/7-scale model of the North American X-15 airplane with and without fuselage forebody strakes /

Hassell, James L.
Hewes, Donald E.
United States. National Aeronautics and Space Administration.

"February 1960."Cover title.Includes bibliographical references (p. 17).Mode of access: Internet

Pressure distribution of a 0.0667-scale model of the X-15 airplane for an angle-of-attack range of 0° to 28° at mach numbers of 2.30, 288, and 4.65 /

Hodge, B. Leon.
Burbank, Paige B.
United States. National Aeronautics and Space Administration.

"May 1960."Cover title.Includes bibliographical references (p. 8).Mode of access: Internet

Stability and control characteristics of a 0.0667-scale model of the final version of the North American X-15 research airplane (configuration 3) at transonic speeds /

Osborne, Robert S.
Ware, George M.
United States. National Aeronautics and Space Administration.

"April 1963."Cover title.Includes bibliographical references (p. 8).Mode of access: Internet

Aerodynamic and landing measurements obtained during the first powered flight of the North American X-15 research airplane /

United States. National Aeronautics and Space Administration.
Flight Research Center (U.S.)

"January 1960."Cover title.Includes bibliographical references (p. 17).Mode of access: Internet

Basic pressure measurements on a 0.0667-scale model of the North American X-15 research airplane at transonic speeds /

Osborne, Robert S.
Stafford, Virginia C.
Langley Research Center.
United States. National Aeronautics and Space Administration.

"Langley Research Center, Langely Field, Va.""October 1960."Cover title.Includes bibliographical ref...

Preliminary base pressures obtained from the X-15 airplane at mach numbers from 1.1 to 3.2 /

Saltzman, Edwin J.
United States. National Aeronautics and Space Administration.

Cover title."August 1961."Aerodynamics, aircraft;Aerodynamics, missiles and space vehicles; Vehicle ...

Launch, low-speed, and landing characteristics determined from the first flight of the North American X-15 research airplane /

Finch, Thomas W.
Matranga, Gene J.
United States. National Aeronautics and Space Administration.

"September 1959."Cover title.Includes bibliographical references (p. 11).Mode of access: Internet

Static longitudinal, directional, and lateral stability and control data at a mach number of 6.83 of the final configuration of the X-15 research airplane /

Penland, Jim A.
Fetterman, Jr., David E.
Langley Research Center.

January 1960

"April 1960"--Cover.Caption title.Includes bibliographical references (p. 10-11).Mode of access: Int...

Landing loads and dynamics of the X-15 airplane /

McKay, James M..
Kordes, Eldon E.
Flight Research Center.

January 1962

"March 1962."Includes bibliographical references (p. 11).Mode of access: Internet

Low-speed measurements of oscillatory lateral stability derivatives of a 1/7-scale model of the North American X-15 airplane /

Paulson, John W.
Hassell, James L.
United States. National Aeronautics and Space Administration.

"November 1959."Cover title.Includes bibliographical references (p. 6).Mode of access: Internet

Aerodynamic loads at mach numbers from 0.70 to 2.22 on an airplane model having a wing and canard of triangular plan form and either single or twin vertical tails /

Peterson, Victor L.
Menees, Gene P.
United States. National Aeronautics and Space Administration.

Cover title."June 1961."Aerodynamics, aircraft; Stresses and loads.Includes bibliographical referenc...

Full-scale wind-tunnel investigation of the aerodynamic characteristics of the X-24A lifting body aircraft /

Mort, Kenneth W.
Falarski, Michael D.
U.S. Army Aeronautical Research Laboratory.
Ames Research Center.
United States. National Aeronautics and Space Administration.

"August 1970."Cover title.Includes bibliographical references (p. 6).Mode of access: Internet

Aerodynamic-derivative characteristics of the X-15 research airplane as determined from flight tests for mach numbers from 0.6 to 3.4 /

Yancey, Roxanah B.
United States. National Aeronautics and Space Administration.

Cover title."January 1962."Aerodynamics, aircraft; Aerodynamics, missiles and space vehicles; Aircra...

Static stability and control characteristics of an airplane model with tail surfaces outboard of the wing tips at a mach number of 2.01 /

Driver, Cornelius.
Spearman, M. Leroy.
United States. National Aeronautics and Space Administration.

"September 1959."Cover title.Includes bibliographical references (p. 8).Mode of access: Internet

Investigation of the loading characteristics of the lifting surfaces and the speed brakes of a 0.067-scale model of the north american x-15 airplane (configuration 3) at Mach numbers of 2.29, 2.98, and 4.65 /

Abstract

Extracted data

Investigation of the loading characteristics of the lifting surfaces and the speed brakes of a 0.067-scale model of the north american x-15 airplane (configuration 3) at Mach numbers of 2.29, 2.98, and 4.65 /

Abstract

Extracted data

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