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 /

Wind-tunnel investigation of the static lateral stability characteristics of wing-fuselage combinations at high supersonic speeds. Aspect-ratio series /

Fournier, Paul G.
Byrnes, Andrew L.
Langley Aeronautical Laboratory.
United States. National Adviosry Committee for Aeronautics. NACA research memorandum.

January 1953

"February 9, 1953."Includes bibliographical references (p. 9).Mode of access: Internet

Investigation of the low-subsonic flight characteristics of a model of a reentry vehicle with a thick flat 75 degree swept delta wing and a half-cone fuselage /

Boisseau, Peter C.
United States. National Aeronautics and Space Administration.

Cover title."February 1962."Aerodynamics, aircraft; Aerodynamics, missiles and space vehicles; Satel...

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

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

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

Wind-tunnel investigation at a Mach number of 2.91 of stability and control characteristics of three lifting reentry configurations at angles of attack up to 90° /

Grimaud, John E.
Langley Research Center.

January 1961

"March 1961."Caption title.Includes bibliographical references (p. 11).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

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

Putnam, Lawrence E. (Lawrence Elwood)
Brooks, Cuyler W.
Langley Research Center.

January 1962

"December 1962."Cover title.Includes bibliographical references (p. 9).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

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

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

Low-subsonic-speed static stability of right-triangular-pyramid and half-cone lifting reentry configurations. /

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

Abstract:Cover title."February 1961."Aerodynamics, missiles and space vehicles; Space vehicles; Stab...

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

Investigation of the low-subsonic stability and control characteristics of a 1/3-scale free-flying model of a lifting-body reentry configuration /

Hassell, James L.
United States. National Aeronautics and Space Administration.

"July 1960."Cover title.Includes bibliographical references (p. 14).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 of the static lateral stability characteristics of wing-fuselage combinations at high supersonic speeds. Aspect-ratio series /

Fournier, Paul G.
Byrnes, Andrew L.
Langley Aeronautical Laboratory.
United States. National Adviosry Committee for Aeronautics. NACA research memorandum.

January 1953

"February 9, 1953."Includes bibliographical references (p. 9).Mode of access: Internet

Investigation of the low-subsonic flight characteristics of a model of a reentry vehicle with a thick flat 75 degree swept delta wing and a half-cone fuselage /

Boisseau, Peter C.
United States. National Aeronautics and Space Administration.

Cover title."February 1962."Aerodynamics, aircraft; Aerodynamics, missiles and space vehicles; Satel...

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

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

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

Wind-tunnel investigation at a Mach number of 2.91 of stability and control characteristics of three lifting reentry configurations at angles of attack up to 90° /

Grimaud, John E.
Langley Research Center.

January 1961

"March 1961."Caption title.Includes bibliographical references (p. 11).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

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

Putnam, Lawrence E. (Lawrence Elwood)
Brooks, Cuyler W.
Langley Research Center.

January 1962

"December 1962."Cover title.Includes bibliographical references (p. 9).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

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

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

Low-subsonic-speed static stability of right-triangular-pyramid and half-cone lifting reentry configurations. /

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

Abstract:Cover title."February 1961."Aerodynamics, missiles and space vehicles; Space vehicles; Stab...

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

Investigation of the low-subsonic stability and control characteristics of a 1/3-scale free-flying model of a lifting-body reentry configuration /

Hassell, James L.
United States. National Aeronautics and Space Administration.

"July 1960."Cover title.Includes bibliographical references (p. 14).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 of the static lateral stability characteristics of wing-fuselage combinations at high supersonic speeds. Aspect-ratio series /

Fournier, Paul G.
Byrnes, Andrew L.
Langley Aeronautical Laboratory.
United States. National Adviosry Committee for Aeronautics. NACA research memorandum.

January 1953

"February 9, 1953."Includes bibliographical references (p. 9).Mode of access: Internet

Investigation of the low-subsonic flight characteristics of a model of a reentry vehicle with a thick flat 75 degree swept delta wing and a half-cone fuselage /

Boisseau, Peter C.
United States. National Aeronautics and Space Administration.

Cover title."February 1962."Aerodynamics, aircraft; Aerodynamics, missiles and space vehicles; Satel...

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

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 /

Abstract

Extracted data

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 /

Abstract

Extracted data

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