Flight-determined derivatives and dynamic characteristics for the HL-10 lifting body vehicle at subsonic and transonic Mach numbers /

Transonic aeroelastic analysis of launch vehicle configurations /

Azevedo, João Luiz Filgueiras de.
Langley Research Center.

January 1988

"Prepared for Langley Research Center under Grant NGL 05-020-243."Bibliography: p. 146-154.Mode of a...

Aerodynamic characteristics of a large aircraft to transport space shuttle orbiter or other external payloads /

Paulson, John W.
Langley Research Center.

January 1975

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

Supersonic dynamic stability characteristics of a space shuttle orbiter /

Freeman, Delma C.
Davenport, Edwin E.
Boyden, Richmond P.
Langley Research Center.

January 1976

Prepared at Langley Research Center.Cover title.Includes bibliographical references (p. 25).Mode of ...

Flight-determined derivatives and dynamic characteristics of the CV-990 airplane /

Gilyard, Glenn B.
Flight Research Center (U.S.)

January 1972

Prepared at NASA Flight Research Center.Cover title.Bibliography: p. 24.Mode of access: Internet

Flight evaluation of HL-10 lifting body handling qualities at Mach numbers from 0.30 to 1.86 /

Kempel, Robert W.
Manke, John A.
United States. National Aeronautics and Space Administration.

January 1974

"January 1974."Cover title.Includes bibliographical references (p. 16).Mode of access: Internet

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 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

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

Subsonic and transonic dynamic-stability characteristics of the space shuttle launch vehicle /

Freeman, Delma C.
Davenport, Edwin E., joint author.
Boyden, Richmond P., joint author.
Langley Research Center.

January 1976

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

Supersonic dynamic-stability derivatives of the space shuttle launch vehicle /

Boyden, Richmond P.
Davenport, Edwin E.
Freeman, Delma C.
Langley Research Center.

January 1976

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

Effects of body shape on the aerodynamic characteristics of an all-body hypersonic aircraft configuration at Mach numbers from 0.65 to 10.6 /

Nelms, Walter P.
Ames Research Center.

January 1972

Prepared at Ames Research Center.Cover title.Bibliography: p. 8-9.Mode of access: Internet

Subsonic and transonic dynamic stability characteristics of a space shuttle orbiter /

Boyden, Richmond P.
Freeman, Delma C.
Langley Research Center.

January 1975

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

Experimental and theoretical aerodynamic characteristics of a high-lift semispan wing model /

Applin, Zachary T.
Gentry, Garl L.
Langley Research Center.

January 1990

Prepared at Langley Research Center.Bibliography: p. 21.Mode of access: Internet

Subsonic roll-damping characteristics of a series of wings /

Boyden, Richmond P.
Langley Research Center.

January 1974

Prepared at Langley Research Center.Cover title.Includes bibliographical references (p. 10-11).Mode ...

Transonic aeroelastic analysis of launch vehicle configurations /

Azevedo, João Luiz Filgueiras de.
Langley Research Center.

January 1988

"Prepared for Langley Research Center under Grant NGL 05-020-243."Bibliography: p. 146-154.Mode of a...

Aerodynamic characteristics of a large aircraft to transport space shuttle orbiter or other external payloads /

Paulson, John W.
Langley Research Center.

January 1975

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

Supersonic dynamic stability characteristics of a space shuttle orbiter /

Freeman, Delma C.
Davenport, Edwin E.
Boyden, Richmond P.
Langley Research Center.

January 1976

Prepared at Langley Research Center.Cover title.Includes bibliographical references (p. 25).Mode of ...

Flight-determined derivatives and dynamic characteristics of the CV-990 airplane /

Gilyard, Glenn B.
Flight Research Center (U.S.)

January 1972

Prepared at NASA Flight Research Center.Cover title.Bibliography: p. 24.Mode of access: Internet

Flight evaluation of HL-10 lifting body handling qualities at Mach numbers from 0.30 to 1.86 /

Kempel, Robert W.
Manke, John A.
United States. National Aeronautics and Space Administration.

January 1974

"January 1974."Cover title.Includes bibliographical references (p. 16).Mode of access: Internet

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 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

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

Subsonic and transonic dynamic-stability characteristics of the space shuttle launch vehicle /

Freeman, Delma C.
Davenport, Edwin E., joint author.
Boyden, Richmond P., joint author.
Langley Research Center.

January 1976

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

Supersonic dynamic-stability derivatives of the space shuttle launch vehicle /

Boyden, Richmond P.
Davenport, Edwin E.
Freeman, Delma C.
Langley Research Center.

January 1976

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

Effects of body shape on the aerodynamic characteristics of an all-body hypersonic aircraft configuration at Mach numbers from 0.65 to 10.6 /

Nelms, Walter P.
Ames Research Center.

January 1972

Prepared at Ames Research Center.Cover title.Bibliography: p. 8-9.Mode of access: Internet

Subsonic and transonic dynamic stability characteristics of a space shuttle orbiter /

Boyden, Richmond P.
Freeman, Delma C.
Langley Research Center.

January 1975

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

Experimental and theoretical aerodynamic characteristics of a high-lift semispan wing model /

Applin, Zachary T.
Gentry, Garl L.
Langley Research Center.

January 1990

Prepared at Langley Research Center.Bibliography: p. 21.Mode of access: Internet

Subsonic roll-damping characteristics of a series of wings /

Boyden, Richmond P.
Langley Research Center.

January 1974

Prepared at Langley Research Center.Cover title.Includes bibliographical references (p. 10-11).Mode ...

Transonic aeroelastic analysis of launch vehicle configurations /

Azevedo, João Luiz Filgueiras de.
Langley Research Center.

January 1988

"Prepared for Langley Research Center under Grant NGL 05-020-243."Bibliography: p. 146-154.Mode of a...

Aerodynamic characteristics of a large aircraft to transport space shuttle orbiter or other external payloads /

Paulson, John W.
Langley Research Center.

January 1975

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

Supersonic dynamic stability characteristics of a space shuttle orbiter /

Freeman, Delma C.
Davenport, Edwin E.
Boyden, Richmond P.
Langley Research Center.

January 1976

Prepared at Langley Research Center.Cover title.Includes bibliographical references (p. 25).Mode of ...

Flight-determined derivatives and dynamic characteristics for the HL-10 lifting body vehicle at subsonic and transonic Mach numbers /

Abstract

Extracted data

Flight-determined derivatives and dynamic characteristics for the HL-10 lifting body vehicle at subsonic and transonic Mach numbers /

Abstract

Extracted data

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