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 /

Wind-tunnel investigation of static aerodynamic characteristics of a 1/9-scale model of a Project Mercury capsule at mach numbers from 1.60 to 4.65 /

Shaw, David S.
Turner, Kenneth L.
United States. National Aeronautics and Space Administration.

"July 1960."Cover title.Includes bibliographical references (p. 7).Mode of access: Internet

Transonic aerodynamic characteristics of a variable-sweep airplane configuration having a 12-percent-thick wing and an inboard pivot location /

Bielat, Ralph P.
Pierpont, P. Kenneth.
Langley Research Center.

January 1960

"December 1960."Cover title.Includes bibliographical references (p. 10).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

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

Sleeman, William C.
Robins, A. Warner.
Langley Research Center.

Cover title.Includes bibliographical references (p. 18).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

Static longitudinal and lateral aerodynamic characteristics at a Mach number of 2.20 of a variable-wing-sweep STOL configuration /

Foster, Gerald V.
Morris, Odell A.
Langley Research Center.
United States. National Aeronautics and Space Administration.

January 1960

"October 1960."Cover title.Includes bibliographical references (p. 7-8).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

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...

Aerodynamic characteristics in pitch at a Mach number of 1.97 of two variable-wing- sweep V/STOL configurations with outboard wing panels swept back 75° /

Foster, Gerald V.
Morris, Odell A.
Langley Research Center.
United States. National Aeronautics and Space Administration.

January 1960

"October 1960."Cover title.Includes bibliographical references (p. 6).Mode of access: Internet

Static longitudinal and lateral aerodynamic characteristics at a Mach number of 2.01 of a tailless delta V/STOL configuration having variable-sweep wing panels /

Spearman, M. Leroy.
Foster, Gerald V.
Langley Research Center.

January 1961

"December 1961."Cover title.Includes bibliographical references (p. 8).Mode of access: Internet

Wind-tunnel investigation of the effects of steady rolling on the aerodynamic loading characteristics of a 45©� sweptback wing at high subsonic speeds /

Wiggins, James W.
Kuhn, Richard E.
Langley Aeronautical Laboratory.
United States. National Adviosry Committee for Aeronautics. NACA research memorandum.
United States. National Advisory Committee for Aeronautics.

January 1954

"November 6, 1953."Cover title.Includes bibliographical references (p. 6).Mode of access: Internet

Wind-tunnel investigation at high subsonic speed of the static longitudinal stability characteristics of a winged reentry vehicle having a large negatively deflected flap-type control surface /

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

"December 1959."Cover title.Includes bibliographical references (p. 7).Mode of access: Internet

Wind-tunnel investigation at Mach numbers from 0.60 to 1.20 of the static aerodynamic characteristics of a model of a possible nonlifting reentry capsule in combination with a rocket booster /

Pearson, Albin O.
Langley Research Center.

January 1960

"September 1960."Cover title.Includes bibliographical references (p. 6).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

Wind-tunnel investigation at mach numbers from 0.50 to 1.14 of the static aerodynamic characteristics of a model of a Project Mercury capsule /

Pearson, Albin O.
United States. National Aeronautics and Space Administration.

"July 1960."Cover title.Includes bibliographical references (p. 6).Mode of access: Internet

Wind-tunnel investigation of static aerodynamic characteristics of a 1/9-scale model of a Project Mercury capsule at mach numbers from 1.60 to 4.65 /

Shaw, David S.
Turner, Kenneth L.
United States. National Aeronautics and Space Administration.

"July 1960."Cover title.Includes bibliographical references (p. 7).Mode of access: Internet

Transonic aerodynamic characteristics of a variable-sweep airplane configuration having a 12-percent-thick wing and an inboard pivot location /

Bielat, Ralph P.
Pierpont, P. Kenneth.
Langley Research Center.

January 1960

"December 1960."Cover title.Includes bibliographical references (p. 10).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

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

Sleeman, William C.
Robins, A. Warner.
Langley Research Center.

Cover title.Includes bibliographical references (p. 18).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

Static longitudinal and lateral aerodynamic characteristics at a Mach number of 2.20 of a variable-wing-sweep STOL configuration /

Foster, Gerald V.
Morris, Odell A.
Langley Research Center.
United States. National Aeronautics and Space Administration.

January 1960

"October 1960."Cover title.Includes bibliographical references (p. 7-8).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

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...

Aerodynamic characteristics in pitch at a Mach number of 1.97 of two variable-wing- sweep V/STOL configurations with outboard wing panels swept back 75° /

Foster, Gerald V.
Morris, Odell A.
Langley Research Center.
United States. National Aeronautics and Space Administration.

January 1960

"October 1960."Cover title.Includes bibliographical references (p. 6).Mode of access: Internet

Static longitudinal and lateral aerodynamic characteristics at a Mach number of 2.01 of a tailless delta V/STOL configuration having variable-sweep wing panels /

Spearman, M. Leroy.
Foster, Gerald V.
Langley Research Center.

January 1961

"December 1961."Cover title.Includes bibliographical references (p. 8).Mode of access: Internet

Wind-tunnel investigation of the effects of steady rolling on the aerodynamic loading characteristics of a 45©� sweptback wing at high subsonic speeds /

Wiggins, James W.
Kuhn, Richard E.
Langley Aeronautical Laboratory.
United States. National Adviosry Committee for Aeronautics. NACA research memorandum.
United States. National Advisory Committee for Aeronautics.

January 1954

"November 6, 1953."Cover title.Includes bibliographical references (p. 6).Mode of access: Internet

Wind-tunnel investigation at high subsonic speed of the static longitudinal stability characteristics of a winged reentry vehicle having a large negatively deflected flap-type control surface /

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

"December 1959."Cover title.Includes bibliographical references (p. 7).Mode of access: Internet

Wind-tunnel investigation at Mach numbers from 0.60 to 1.20 of the static aerodynamic characteristics of a model of a possible nonlifting reentry capsule in combination with a rocket booster /

Pearson, Albin O.
Langley Research Center.

January 1960

"September 1960."Cover title.Includes bibliographical references (p. 6).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

Wind-tunnel investigation at mach numbers from 0.50 to 1.14 of the static aerodynamic characteristics of a model of a Project Mercury capsule /

Pearson, Albin O.
United States. National Aeronautics and Space Administration.

"July 1960."Cover title.Includes bibliographical references (p. 6).Mode of access: Internet

Wind-tunnel investigation of static aerodynamic characteristics of a 1/9-scale model of a Project Mercury capsule at mach numbers from 1.60 to 4.65 /

Shaw, David S.
Turner, Kenneth L.
United States. National Aeronautics and Space Administration.

"July 1960."Cover title.Includes bibliographical references (p. 7).Mode of access: Internet

Transonic aerodynamic characteristics of a variable-sweep airplane configuration having a 12-percent-thick wing and an inboard pivot location /

Bielat, Ralph P.
Pierpont, P. Kenneth.
Langley Research Center.

January 1960

"December 1960."Cover title.Includes bibliographical references (p. 10).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 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 /

Abstract

Extracted data

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 /

Abstract

Extracted data

Related items

Related items