Investigation of low-subsonic flight characteristics of a model of a hypersonic boost-glide configuration having a 78 degree delta wing /by /

An analysis of the delta-wing hypersonic stability and control behavior at angles of attack between 30 degrees and 90 degrees

Fetterman, David E.
Neal, Luther.
United States. National Aeronautics and Space Administration.

Cover title."March 1963."Includes bibliographical references.Mode of access: Internet

Aerodynamic characteristics of a canard and an outboard-tail airplane model at high subsonic speeds /

Fournier, Paul G.
United States. National Aeronautics and Space Administration.

Cover title."November 1961."Aerodynamics, aircraft; Aircraft; Stability and control.Includes bibliog...

Investigation at high subsonic speeds of the use of low auxiliary tail surfaces having dihedral to improve the longitudinal and directional stability of a T-tail model at high lift. /

Sleeman, William C.
United States. National Aeronautics and Space Administration.

Cover title."April 1961."Aerodynamics, aircraft; Aircraft; Stability and control.Includes bibliograp...

Investigation of low-subsonic flight characteristics of a model of a hypersonic boost-glide configuration having a 78 degree delta wing /by /

Paulson, John W.
Shanks, Robert E.
United States. National Aeronautics and Space Administration.

Cover title."May 1961."Aerodynamics, aircraft; Aerodynamics, missiles and space vehicles; Stability ...

High-subsonic-speed investigation of the static longitudinal aerodynamic characteristics of several delta-wing configurations for angles of attack from 0° to 90° /

Spencer, Bernard, 1932-
Langley Research Center.
United States. National Aeronautics and Space Administration.

January 1959

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

Investigation of the low-subsonic stability and control characteristics of a 1/3-scale free-flying model of a lifting-body reentry configuration /

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

"July 1960."Cover title.Includes bibliographical references (p. 14).Mode of access: Internet

Low-speed aerodynamic characteristics of a model of a hypersonic research airplane at angles of attack up to 90 degrees for a range of Reynolds numbers /

Bowman, James S.
Grantham, William D.
United States. National Aeronautics and Space Administration.

Cover title."September 1960."Aerodynamics, aircraft;Aircraft; Stability and control;Includes biblio...

Investigation of the low-subsonic flight characteristics of a model of a reentry vehicle with a thick flat 75 degree swept delta wing and a half-cone fuselage /

Boisseau, Peter C.
United States. National Aeronautics and Space Administration.

Cover title."February 1962."Aerodynamics, aircraft; Aerodynamics, missiles and space vehicles; Satel...

Investigation of the low-subsonic aerodynamic characteristics of a model of a modified lenticular reentry configuration /

Ware, George M.
Langley Research Center.

January 1962

"December 1962."Cover title.Includes bibliographical references (p. 10).Mode of access: Internet

Hypersonic longitudinal trim, stability, and control characteristics of a delta-wing configuration at high angles of attack /

Close, William H.
United States. National Aeronautics and Space Administration.

"April 1960."Cover title.Includes bibliographical references (p. 16).Mode of access: Internet

Investigation of the low-subsonic stability and control characteristics of a free-flying model of a thick 70 degree Delta reentrry configuration /

Paulson, John W.
Shanks, Robert E.
United States. National Aeronautics and Space Administration.

Cover title."October 1961."Major NASA subject terms: Aerodynamics, missiles and space vehicles; Stab...

Low-speed investigation of a full-span internal-flow jet-augmented flap on a high-wing model with a 35 degree swept wing of aspect ratio 7.0 /

Turner, Thomas R.
United States. National Aeronautics and Space Administration.

Cover title."August 1960."Aerodynamics, aircraft, Aircraft; Stability and control.Includes bibliogra...

Experimental low-speed and calculated high-speed aerodynamic characteristics of a hypersonic research airplane concept having a 65 ̊swept delta wing /

Penland, Jim A.
Howard, Floyd G.
Creel, Theodore R.
Langley Research Center.

January 1974

Prepared at Langley Research Center.Cover title.Includes bibliographical references (p. 12).Mode of ...

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

Subsonic aerodynamic characteristics of an airplane configuration utilizing a variable-sweep wing having a free-floating apex /

Polhamus, Edward C., 1948-
Hammond, Alexander D.
Langley Research Center.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.

January 1965

"July 1965"--Cover.Cover title.Includes bibliographical references (p. 9).Mode of access: Internet

An analysis of the delta-wing hypersonic stability and control behavior at angles of attack between 30 degrees and 90 degrees

Fetterman, David E.
Neal, Luther.
United States. National Aeronautics and Space Administration.

Cover title."March 1963."Includes bibliographical references.Mode of access: Internet

Aerodynamic characteristics of a canard and an outboard-tail airplane model at high subsonic speeds /

Fournier, Paul G.
United States. National Aeronautics and Space Administration.

Cover title."November 1961."Aerodynamics, aircraft; Aircraft; Stability and control.Includes bibliog...

Investigation at high subsonic speeds of the use of low auxiliary tail surfaces having dihedral to improve the longitudinal and directional stability of a T-tail model at high lift. /

Sleeman, William C.
United States. National Aeronautics and Space Administration.

Cover title."April 1961."Aerodynamics, aircraft; Aircraft; Stability and control.Includes bibliograp...

Investigation of low-subsonic flight characteristics of a model of a hypersonic boost-glide configuration having a 78 degree delta wing /by /

Paulson, John W.
Shanks, Robert E.
United States. National Aeronautics and Space Administration.

Cover title."May 1961."Aerodynamics, aircraft; Aerodynamics, missiles and space vehicles; Stability ...

High-subsonic-speed investigation of the static longitudinal aerodynamic characteristics of several delta-wing configurations for angles of attack from 0° to 90° /

Spencer, Bernard, 1932-
Langley Research Center.
United States. National Aeronautics and Space Administration.

January 1959

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

Investigation of the low-subsonic stability and control characteristics of a 1/3-scale free-flying model of a lifting-body reentry configuration /

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

"July 1960."Cover title.Includes bibliographical references (p. 14).Mode of access: Internet

Low-speed aerodynamic characteristics of a model of a hypersonic research airplane at angles of attack up to 90 degrees for a range of Reynolds numbers /

Bowman, James S.
Grantham, William D.
United States. National Aeronautics and Space Administration.

Cover title."September 1960."Aerodynamics, aircraft;Aircraft; Stability and control;Includes biblio...

Investigation of the low-subsonic flight characteristics of a model of a reentry vehicle with a thick flat 75 degree swept delta wing and a half-cone fuselage /

Boisseau, Peter C.
United States. National Aeronautics and Space Administration.

Cover title."February 1962."Aerodynamics, aircraft; Aerodynamics, missiles and space vehicles; Satel...

Investigation of the low-subsonic aerodynamic characteristics of a model of a modified lenticular reentry configuration /

Ware, George M.
Langley Research Center.

January 1962

"December 1962."Cover title.Includes bibliographical references (p. 10).Mode of access: Internet

Hypersonic longitudinal trim, stability, and control characteristics of a delta-wing configuration at high angles of attack /

Close, William H.
United States. National Aeronautics and Space Administration.

"April 1960."Cover title.Includes bibliographical references (p. 16).Mode of access: Internet

Investigation of the low-subsonic stability and control characteristics of a free-flying model of a thick 70 degree Delta reentrry configuration /

Paulson, John W.
Shanks, Robert E.
United States. National Aeronautics and Space Administration.

Cover title."October 1961."Major NASA subject terms: Aerodynamics, missiles and space vehicles; Stab...

Low-speed investigation of a full-span internal-flow jet-augmented flap on a high-wing model with a 35 degree swept wing of aspect ratio 7.0 /

Turner, Thomas R.
United States. National Aeronautics and Space Administration.

Cover title."August 1960."Aerodynamics, aircraft, Aircraft; Stability and control.Includes bibliogra...

Experimental low-speed and calculated high-speed aerodynamic characteristics of a hypersonic research airplane concept having a 65 ̊swept delta wing /

Penland, Jim A.
Howard, Floyd G.
Creel, Theodore R.
Langley Research Center.

January 1974

Prepared at Langley Research Center.Cover title.Includes bibliographical references (p. 12).Mode of ...

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

Subsonic aerodynamic characteristics of an airplane configuration utilizing a variable-sweep wing having a free-floating apex /

Polhamus, Edward C., 1948-
Hammond, Alexander D.
Langley Research Center.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.

January 1965

"July 1965"--Cover.Cover title.Includes bibliographical references (p. 9).Mode of access: Internet

An analysis of the delta-wing hypersonic stability and control behavior at angles of attack between 30 degrees and 90 degrees

Fetterman, David E.
Neal, Luther.
United States. National Aeronautics and Space Administration.

Cover title."March 1963."Includes bibliographical references.Mode of access: Internet

Aerodynamic characteristics of a canard and an outboard-tail airplane model at high subsonic speeds /

Fournier, Paul G.
United States. National Aeronautics and Space Administration.

Cover title."November 1961."Aerodynamics, aircraft; Aircraft; Stability and control.Includes bibliog...

Investigation at high subsonic speeds of the use of low auxiliary tail surfaces having dihedral to improve the longitudinal and directional stability of a T-tail model at high lift. /

Sleeman, William C.
United States. National Aeronautics and Space Administration.

Cover title."April 1961."Aerodynamics, aircraft; Aircraft; Stability and control.Includes bibliograp...

Investigation of low-subsonic flight characteristics of a model of a hypersonic boost-glide configuration having a 78 degree delta wing /by /

Abstract

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Investigation of low-subsonic flight characteristics of a model of a hypersonic boost-glide configuration having a 78 degree delta wing /by /

Abstract

Extracted data

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