Low-speed investigation of the aerodynamic characteristics of a variable-sweep supersonic transport configuration having a blended wing and body /

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.

January 1959

Cover title."October 1959."Includes bibliographical references.Mode of access: Internet

Low subsonic flight and force investigation of a supersonic transport model with a highly swept arrow wing /

Freeman, Delma C.
Langley Research Center.

January 1967

Work performed at Langley Research Center.Includes bibliographical references (p. 19).Mode of access...

Flutter analysis of swept-wing subsonic aircraft with parameter studies of composite wings /

Housner, Jerrold M.
Stein, Manuel.
Langley Research Center.

January 1974

Prepared at Langley Research Center.Cover title.Includes bibliographical references (p. 93).Mode of ...

Low-speed characteristics of a variable-sweep supersonic transport model with a blended engine fuselage and engine-mounted tails /

Lockwood, Vernard E.
Thompson, Wilson E.
Langley Research Center.

January 1964

"November 1964."Includes bibliographical references (p. 10).Mode of access: Internet

Low-speed longitudinal stability characteristics of a supersonic transport configuration with variable-sweep wings employing a double inboard pivot /

Henderson, William P.
Langley Research Center.

Cover title.Includes bibliographical references (p. 9-10).Mode of access: Internet

Wind-tunnel investigation at Mach numbers from 1.60 to 2.86 of the static aerodynamic characteristics of a supersonic transport configuration with variable-sweep wings employing a double inboard pivot /

Shaw, David S.
Henderson, William P.
Langley Research Center.

Cover title.Includes bibliographical references (p. 12).Mode of access: Internet

Aerodynamic characteristics of a three-engine supersonic transport model having a low-aspect-ratio variable-sweep warped wing /

Morris, Odell A.
Fuller, Dennis E.
Langley Research Center.

January 1964

"September 1964."Includes bibliographical references (p. 9).Mode of access: Internet

Wind-tunnel studies at subsonic and transonic speeds of a multiple-mission variable-wing- sweep airplane configuration /

Alford, William J.
Handerson, William P.
Luoma, Arvo A.
Langley Research Center.

January 1959

"November 1959."Cover title.Includes bibliographical references (p. 13).Mode of access: Internet

Investigation of pitch maneuver speed margins for a supersonic transport configuration with a variable-sweep wing /

Sawyer, Richard H.
Silsby, Norman S.
McLaughlin, Milton D.
United States. National Aeronautics and Space Administration.
Langley Research Center.

January 1967

"October 1967."Includes bibliographical references (p. 15).Mode of access: Internet

Low subsonic flight and force investigation of a supersonic transport model with a variable-sweep wing /

Freeman, Delma C., Jr.
Langley Research Center.
United States. National Aeronautics and Space Administration.

January 1968

Work performed at Langley Research Center.N69-10733.Includes bibliographical references (p. 15).Mode...

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

Cook, Anthony M.
Ames Research Center.
United States. National Aeronautics and Space Administration.

January 1968

Work performed at Ames Research Center.N68-37365.Includes bibliographical references (p. 12).Mode of...

The transonic aerodynamic characteristics of two variable-sweep airplane configurations capable of low-level supersonic attack /

Bielat, Ralph P.
Alford, William J.
Robins, A. Warner.
Langley Research Center.

January 1960

"August 1960."Cover title.Includes bibliographical references (p. 11-12).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

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 ...

Low-speed aerodynamic characteristics of an airfoil optimized for maximum lift coefficient /

Bingham, Gene J.
Chen, Allen Wen-shin, 1945-
Langley Research Center.

January 1972

Prepared at Langley Research Center.Cover title.Bibliography: p. 13.Mode of access: Internet

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.

January 1959

Cover title."October 1959."Includes bibliographical references.Mode of access: Internet

Low subsonic flight and force investigation of a supersonic transport model with a highly swept arrow wing /

Freeman, Delma C.
Langley Research Center.

January 1967

Work performed at Langley Research Center.Includes bibliographical references (p. 19).Mode of access...

Flutter analysis of swept-wing subsonic aircraft with parameter studies of composite wings /

Housner, Jerrold M.
Stein, Manuel.
Langley Research Center.

January 1974

Prepared at Langley Research Center.Cover title.Includes bibliographical references (p. 93).Mode of ...

Low-speed characteristics of a variable-sweep supersonic transport model with a blended engine fuselage and engine-mounted tails /

Lockwood, Vernard E.
Thompson, Wilson E.
Langley Research Center.

January 1964

"November 1964."Includes bibliographical references (p. 10).Mode of access: Internet

Low-speed longitudinal stability characteristics of a supersonic transport configuration with variable-sweep wings employing a double inboard pivot /

Henderson, William P.
Langley Research Center.

Cover title.Includes bibliographical references (p. 9-10).Mode of access: Internet

Wind-tunnel investigation at Mach numbers from 1.60 to 2.86 of the static aerodynamic characteristics of a supersonic transport configuration with variable-sweep wings employing a double inboard pivot /

Shaw, David S.
Henderson, William P.
Langley Research Center.

Cover title.Includes bibliographical references (p. 12).Mode of access: Internet

Aerodynamic characteristics of a three-engine supersonic transport model having a low-aspect-ratio variable-sweep warped wing /

Morris, Odell A.
Fuller, Dennis E.
Langley Research Center.

January 1964

"September 1964."Includes bibliographical references (p. 9).Mode of access: Internet

Wind-tunnel studies at subsonic and transonic speeds of a multiple-mission variable-wing- sweep airplane configuration /

Alford, William J.
Handerson, William P.
Luoma, Arvo A.
Langley Research Center.

January 1959

"November 1959."Cover title.Includes bibliographical references (p. 13).Mode of access: Internet

Investigation of pitch maneuver speed margins for a supersonic transport configuration with a variable-sweep wing /

Sawyer, Richard H.
Silsby, Norman S.
McLaughlin, Milton D.
United States. National Aeronautics and Space Administration.
Langley Research Center.

January 1967

"October 1967."Includes bibliographical references (p. 15).Mode of access: Internet

Low subsonic flight and force investigation of a supersonic transport model with a variable-sweep wing /

Freeman, Delma C., Jr.
Langley Research Center.
United States. National Aeronautics and Space Administration.

January 1968

Work performed at Langley Research Center.N69-10733.Includes bibliographical references (p. 15).Mode...

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

Cook, Anthony M.
Ames Research Center.
United States. National Aeronautics and Space Administration.

January 1968

Work performed at Ames Research Center.N68-37365.Includes bibliographical references (p. 12).Mode of...

The transonic aerodynamic characteristics of two variable-sweep airplane configurations capable of low-level supersonic attack /

Bielat, Ralph P.
Alford, William J.
Robins, A. Warner.
Langley Research Center.

January 1960

"August 1960."Cover title.Includes bibliographical references (p. 11-12).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

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 ...

Low-speed aerodynamic characteristics of an airfoil optimized for maximum lift coefficient /

Bingham, Gene J.
Chen, Allen Wen-shin, 1945-
Langley Research Center.

January 1972

Prepared at Langley Research Center.Cover title.Bibliography: p. 13.Mode of access: Internet

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.

January 1959

Cover title."October 1959."Includes bibliographical references.Mode of access: Internet

Low subsonic flight and force investigation of a supersonic transport model with a highly swept arrow wing /

Freeman, Delma C.
Langley Research Center.

January 1967

Work performed at Langley Research Center.Includes bibliographical references (p. 19).Mode of access...

Flutter analysis of swept-wing subsonic aircraft with parameter studies of composite wings /

Housner, Jerrold M.
Stein, Manuel.
Langley Research Center.

January 1974

Prepared at Langley Research Center.Cover title.Includes bibliographical references (p. 93).Mode of ...

Low-speed investigation of the aerodynamic characteristics of a variable-sweep supersonic transport configuration having a blended wing and body /

Abstract

Extracted data

Low-speed investigation of the aerodynamic characteristics of a variable-sweep supersonic transport configuration having a blended wing and body /

Abstract

Extracted data

Related items

Related items