Aerodynamic testing technique for twin-fuselage models at hypersonic speeds /

Pressure measurements of the leading edge of a swept wing at Mach 2.2 /

Sorrells, Russell B.
Langley Research Center.

January 1974

Prepared at Langley Research Center.Cover title.Includes bibliographical references (p. 11).Mode of ...

Interference between exhaust system and afterbody of twin-engine fuselage configurations /

Runckel, Jack F.
Langley Research Center.

January 1974

Prepared at Langley Research Center.Cover title.Includes bibliographical references (p. 16-17).Mode ...

Aerodynamic roll damping of a T-tail transport configuration /

Boyden, Richmond P.
Langley Research Center.

January 1974

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

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 ...

Numerical methods for the design and analysis of wings at supersonic speeds /

Carlson, Harry W.
Miller, David S.
Langley Research Center.

January 1974

Prepared at Langley Research Center.Cover title.Includes bibliographical references (p. 29-30).Mode ...

Wind-tunnel investigation of a twin-engine straight-wing upper-surface blown jet-flap configuration /

Phelps, Arthur E.
Langley Research Center.

January 1975

Prepared at Langley Research Center.Cover title.Includes bibliographical references (p. 15).Mode of ...

Analysis of transonic flow about lifting wing-body configurations /

Barnwell, Richard W.
Langley Research Center.

January 1975

Prepared at Langley Research Center.Cover title.Includes bibliographical references (p. 69-71).Mode ...

Exploratory tests of two strut fuel injectors for supersonic combustion /

Anderson, Griffin Y.
Gooderum, Paul B.
Langley Research Center.

January 1974

Prepared at Langley Research Center.Cover title.Includes bibliographical references (p. 21).Mode of ...

Supersonic flutter of panels loaded with inplane shear /

Sawyer, James Wayne, 1941-
Langely Research Center.

January 1975

Prepared at Langley Research Center.Cover title.Includes bibliographical references (p. 16).Mode of ...

Subsonic wind-tunnel investigation of a twin-engine attack airplane model having nonmetric powered nacelles /

Lockwood, Vernard E.
Matarazzo, Aniello.
Langley Research Center.

January 1974

Prepared at Langley Research Center.Cover title.Includes bibliographical references (p. 13).Mode of ...

Hypersonic aerodynamic characteristics of a family of power-law, wing-body configuratioons /

Townsend, James C. (James Courtland), 1938-
Langley Research Center.

January 1973

Prepared at Langley Research Center.Cover title.Includes bibliographical references (p. 33-34).Mode ...

Low-speed aerodynamic characteristics of a twin-engine general aviation configuration with aft-fuselage-mounted pusher propellers /

Dunham, Dana Morris.
Langley Research Center.

January 1987

Prepared at Langley Research Center."October 1987"--Cover.Includes bibliographical references (p. 57...

Theoretical and experimental investigation of supersonic aerodynamic characteristics of a twin-fuselage concept /

Wood, Richard M.
Brentner, Kenneth S.
Miller, D. S. (David S.)
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.

January 1983

Distributed to depository libraries in microfiche."August 1983"--Cover.Subject category 02.Includes ...

Supersonic aerodynamics of delta wings /

Wood, Richard M.
Langley Research Center.

January 1988

Prepared at Langley Research Center."March 1988"--Cover.Includes bibliographical references (p. 22-2...

Hypersonic aerodynamics and entry-maneuver--aerothermodynamic interactions for two lifting entry vehicles /

Arrington, James P.
Woods, William C.
Langley Research Center.

January 1972

Prepared at Langley Research Center.Cover title.Bibliography: p. 12.Mode of access: Internet

Pressure measurements of the leading edge of a swept wing at Mach 2.2 /

Sorrells, Russell B.
Langley Research Center.

January 1974

Prepared at Langley Research Center.Cover title.Includes bibliographical references (p. 11).Mode of ...

Interference between exhaust system and afterbody of twin-engine fuselage configurations /

Runckel, Jack F.
Langley Research Center.

January 1974

Prepared at Langley Research Center.Cover title.Includes bibliographical references (p. 16-17).Mode ...

Aerodynamic roll damping of a T-tail transport configuration /

Boyden, Richmond P.
Langley Research Center.

January 1974

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

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 ...

Numerical methods for the design and analysis of wings at supersonic speeds /

Carlson, Harry W.
Miller, David S.
Langley Research Center.

January 1974

Prepared at Langley Research Center.Cover title.Includes bibliographical references (p. 29-30).Mode ...

Wind-tunnel investigation of a twin-engine straight-wing upper-surface blown jet-flap configuration /

Phelps, Arthur E.
Langley Research Center.

January 1975

Prepared at Langley Research Center.Cover title.Includes bibliographical references (p. 15).Mode of ...

Analysis of transonic flow about lifting wing-body configurations /

Barnwell, Richard W.
Langley Research Center.

January 1975

Prepared at Langley Research Center.Cover title.Includes bibliographical references (p. 69-71).Mode ...

Exploratory tests of two strut fuel injectors for supersonic combustion /

Anderson, Griffin Y.
Gooderum, Paul B.
Langley Research Center.

January 1974

Prepared at Langley Research Center.Cover title.Includes bibliographical references (p. 21).Mode of ...

Supersonic flutter of panels loaded with inplane shear /

Sawyer, James Wayne, 1941-
Langely Research Center.

January 1975

Prepared at Langley Research Center.Cover title.Includes bibliographical references (p. 16).Mode of ...

Subsonic wind-tunnel investigation of a twin-engine attack airplane model having nonmetric powered nacelles /

Lockwood, Vernard E.
Matarazzo, Aniello.
Langley Research Center.

January 1974

Prepared at Langley Research Center.Cover title.Includes bibliographical references (p. 13).Mode of ...

Hypersonic aerodynamic characteristics of a family of power-law, wing-body configuratioons /

Townsend, James C. (James Courtland), 1938-
Langley Research Center.

January 1973

Prepared at Langley Research Center.Cover title.Includes bibliographical references (p. 33-34).Mode ...

Low-speed aerodynamic characteristics of a twin-engine general aviation configuration with aft-fuselage-mounted pusher propellers /

Dunham, Dana Morris.
Langley Research Center.

January 1987

Prepared at Langley Research Center."October 1987"--Cover.Includes bibliographical references (p. 57...

Theoretical and experimental investigation of supersonic aerodynamic characteristics of a twin-fuselage concept /

Wood, Richard M.
Brentner, Kenneth S.
Miller, D. S. (David S.)
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.

January 1983

Distributed to depository libraries in microfiche."August 1983"--Cover.Subject category 02.Includes ...

Supersonic aerodynamics of delta wings /

Wood, Richard M.
Langley Research Center.

January 1988

Prepared at Langley Research Center."March 1988"--Cover.Includes bibliographical references (p. 22-2...

Hypersonic aerodynamics and entry-maneuver--aerothermodynamic interactions for two lifting entry vehicles /

Arrington, James P.
Woods, William C.
Langley Research Center.

January 1972

Prepared at Langley Research Center.Cover title.Bibliography: p. 12.Mode of access: Internet

Pressure measurements of the leading edge of a swept wing at Mach 2.2 /

Sorrells, Russell B.
Langley Research Center.

January 1974

Prepared at Langley Research Center.Cover title.Includes bibliographical references (p. 11).Mode of ...

Interference between exhaust system and afterbody of twin-engine fuselage configurations /

Runckel, Jack F.
Langley Research Center.

January 1974

Prepared at Langley Research Center.Cover title.Includes bibliographical references (p. 16-17).Mode ...

Aerodynamic roll damping of a T-tail transport configuration /

Boyden, Richmond P.
Langley Research Center.

January 1974

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

Aerodynamic testing technique for twin-fuselage models at hypersonic speeds /

Abstract

Extracted data

Aerodynamic testing technique for twin-fuselage models at hypersonic speeds /

Abstract

Extracted data

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