Static longitudinal aerodynamic characteristics at a Mach number of 10.03 of low-aspect-ratio wing-body configurations suitable for reentry /

Low speed static longitudinal and lateral aerodynamic characteristics of a model with a low-aspect-ratio variable-incidence wing and with a free-floating and a programed high-lift canard control /

Scallion, William I.
United States. National Aeronautics and Space Administration.

Cover title."October 1962."Aerodynamics, aircraft; Aircraft; Stability and control.Includes biblio...

The lateral and directional aerodynamic characteristics of a re-entry configuration based on a blunt 13° half cone at Mach numbers to 0.90 /

Kenyon, George C.
Ames Research Center.

January 1961

"November 1961."Cover title.Includes bibliographical references (p. 10).Mode of access: Internet

Longitudinal aerodynamic characteristics of several high-drag bodies at Mach numbers from 1.50 to 4.63 /

Campbell, James F.
United States. National Aeronautics and Space Administration.

Cover title."April 1967."Includes bibliographical references.Mode of access: Internet

Static longitudinal aerodynamic characteristics at transonic speeds of a lenticular-shaped reentry vehicle /

Mugler, John P.
Olstad, Walter B.
United States. National Aeronautics and Space Administration.

"December 1960."Cover title.Includes bibliographical references (p. 11).Mode of access: Internet

Low-subsonic-speed static longitudinal stability and control characteristics of a winged reentry-vehicle configuration having wingtip panels that fold up for high-drag reentry /

Ware, George M.
United States. National Aeronautics and Space Administration.

"February 1960."Cover title.Includes bibliographical references (p. 5).Mode of access: Internet

Static longitudinal aerodynamic characteristics at transonic speeds and angles of attack up to 99° of a reentry glider having folding wing-tip panels /

Olstad, Walter B.
Langley Research Center.

January 1961

"October 1961."Cover title.Includes bibliographical references (p. 10-11).Mode of access: Internet

Transonic investigation of the static longitudinal aerodynamic characteristics of low-aspect-ratio wing-body configurations at angles of attack from 0⁰ to 90⁰ /

Trescot, Charles D.
Brooks, Cuyler W.
Putman, Lawrence E.
United States. National Aeronautics and Space Administration.

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

Aerodynamic characteristics of three axismmetric low-fitness-ratio reentry shapes at Mach 6.9 /

Penland, Jim A.
Bernot, Peter T.
United States. National Aeronautics and Space Administration.

January 1967

Cover title."August 1967."Includes bibliographical references (p. 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

Exploratory investigation at mach number of 2.01 of the longitudinal stability and control characteristics of a winged reentry configuration /

Foster, Gerald V.
United States. National Aeronautics and Space Administration.

"December 1959."Cover title.Includes bibliographical references (p. 7).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

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

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

Static longitudinal stability characteristics of a blunted glider reentry configuration having 79.5° sweepback and 45° dihedral at mach number of 6.2 and angles of attack up to 20° /

Mayo, Edward E.
United States. National Aeronautics and Space Administration.

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

Low-speed longitudinal aerodynamic characteristics associated with a series of low-aspect-ration wings having variations in leading contour / Bernard Spencer Jr. and Alexander D. Hammond.

Spencer, Bernard.
Hammond, Alexander D.
United States. National Aeronautics and Space Administration.

Cover title."September 1962."Aerodynamics, missiles and space vehicles; Atmospheric entry; Satellite...

Low speed static longitudinal and lateral aerodynamic characteristics of a model with a low-aspect-ratio variable-incidence wing and with a free-floating and a programed high-lift canard control /

Scallion, William I.
United States. National Aeronautics and Space Administration.

Cover title."October 1962."Aerodynamics, aircraft; Aircraft; Stability and control.Includes biblio...

The lateral and directional aerodynamic characteristics of a re-entry configuration based on a blunt 13° half cone at Mach numbers to 0.90 /

Kenyon, George C.
Ames Research Center.

January 1961

"November 1961."Cover title.Includes bibliographical references (p. 10).Mode of access: Internet

Longitudinal aerodynamic characteristics of several high-drag bodies at Mach numbers from 1.50 to 4.63 /

Campbell, James F.
United States. National Aeronautics and Space Administration.

Cover title."April 1967."Includes bibliographical references.Mode of access: Internet

Static longitudinal aerodynamic characteristics at transonic speeds of a lenticular-shaped reentry vehicle /

Mugler, John P.
Olstad, Walter B.
United States. National Aeronautics and Space Administration.

"December 1960."Cover title.Includes bibliographical references (p. 11).Mode of access: Internet

Low-subsonic-speed static longitudinal stability and control characteristics of a winged reentry-vehicle configuration having wingtip panels that fold up for high-drag reentry /

Ware, George M.
United States. National Aeronautics and Space Administration.

"February 1960."Cover title.Includes bibliographical references (p. 5).Mode of access: Internet

Static longitudinal aerodynamic characteristics at transonic speeds and angles of attack up to 99° of a reentry glider having folding wing-tip panels /

Olstad, Walter B.
Langley Research Center.

January 1961

"October 1961."Cover title.Includes bibliographical references (p. 10-11).Mode of access: Internet

Transonic investigation of the static longitudinal aerodynamic characteristics of low-aspect-ratio wing-body configurations at angles of attack from 0⁰ to 90⁰ /

Trescot, Charles D.
Brooks, Cuyler W.
Putman, Lawrence E.
United States. National Aeronautics and Space Administration.

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

Aerodynamic characteristics of three axismmetric low-fitness-ratio reentry shapes at Mach 6.9 /

Penland, Jim A.
Bernot, Peter T.
United States. National Aeronautics and Space Administration.

January 1967

Cover title."August 1967."Includes bibliographical references (p. 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

Exploratory investigation at mach number of 2.01 of the longitudinal stability and control characteristics of a winged reentry configuration /

Foster, Gerald V.
United States. National Aeronautics and Space Administration.

"December 1959."Cover title.Includes bibliographical references (p. 7).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

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

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

Static longitudinal stability characteristics of a blunted glider reentry configuration having 79.5° sweepback and 45° dihedral at mach number of 6.2 and angles of attack up to 20° /

Mayo, Edward E.
United States. National Aeronautics and Space Administration.

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

Low-speed longitudinal aerodynamic characteristics associated with a series of low-aspect-ration wings having variations in leading contour / Bernard Spencer Jr. and Alexander D. Hammond.

Spencer, Bernard.
Hammond, Alexander D.
United States. National Aeronautics and Space Administration.

Cover title."September 1962."Aerodynamics, missiles and space vehicles; Atmospheric entry; Satellite...

Low speed static longitudinal and lateral aerodynamic characteristics of a model with a low-aspect-ratio variable-incidence wing and with a free-floating and a programed high-lift canard control /

Scallion, William I.
United States. National Aeronautics and Space Administration.

Cover title."October 1962."Aerodynamics, aircraft; Aircraft; Stability and control.Includes biblio...

The lateral and directional aerodynamic characteristics of a re-entry configuration based on a blunt 13° half cone at Mach numbers to 0.90 /

Kenyon, George C.
Ames Research Center.

January 1961

"November 1961."Cover title.Includes bibliographical references (p. 10).Mode of access: Internet

Longitudinal aerodynamic characteristics of several high-drag bodies at Mach numbers from 1.50 to 4.63 /

Campbell, James F.
United States. National Aeronautics and Space Administration.

Cover title."April 1967."Includes bibliographical references.Mode of access: Internet

Static longitudinal aerodynamic characteristics at a Mach number of 10.03 of low-aspect-ratio wing-body configurations suitable for reentry /

Abstract

Extracted data

Static longitudinal aerodynamic characteristics at a Mach number of 10.03 of low-aspect-ratio wing-body configurations suitable for reentry /

Abstract

Extracted data

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