A preliminary investigation of modified blunt 13° half-cone re-entry configurations at subsonic speeds /

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...

Experimental investigation of the transonic flutter of simple thin truncated-cone panels /

Gilman, Jean.
Langley Research Center.

January 1961

"October 1961."Cover title.Includes bibliographical references (p. 13).Mode of access: Internet

Design guide for pitch-up evaluation and investigation at high subsonic speeds of possible limitations due to wing-aspect-ratio variations /

Spreemann, Kenneth P.
United States. National Aeronautics and Space Administration.

"August 1959."Cover title.Includes bibliographical references (p. 14-16).Mode of access: Internet

Experimental investigation of a disk-shaped reentry configuration at transonic and low supersonic speeds /

Lazzeroni, Frank A.
United States. National Aeronautics and Space Administration.

"May 1962."Cover title.Includes bibliographical references (p. 7).Mode of access: Internet

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

Investigation of the low-subsonic stability and control characteristics of a 0.34-scale free-flying model of a modified half-cone reentry vehicle /

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

"January 1962."Cover title.Includes bibliographical references (p. 15).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

Aerodynamic characteristics of a modified cone : conical-frustum entry configuration at Mach 6.0 /

Ashby, George C.
Staylor, W. Frank.
Langley Research Center.
United States. National Aeronautics and Space Administration.

January 1968

Cover title."June 1968."Includes bibliographical references (p. 8).Mode of access: Internet

Subsonic aerodynamic characteristics of disk re-entry configurations with elliptic cross sections and thickness-diameter ratios of 0.225 and 0.325 /

Demele, Fred A.
Brownson, Jack J.
United States. National Aeronautics and Space Administration.

"May 1961."Cover title.Includes bibliographical references (p. 9-10).Mode of access: Internet

Investigation of a retrorocket exhausting from the nose of a blunt body into a supersonic free stream /

Charczenko, Nickolai.
Hennessey, Katherine W.
United States. National Aeronautics and Space Administration.

Cover title."September 1961."Aerodynamics, missiles and space vehicles; Atmospheric entry.Includes b...

Investigation of an underslung half-cone inlet with compression surface mounted outboard from fuselage at mach numbers of 1.5, 1.8, and 2.0 /

Yeager, Richard A.
Gertsma, Laurence W.
Lewis Flight Propulsion Laboratory.
United States. National Adviosry Committee for Aeronautics. NACA research memorandum.

January 1958

"May 12, 1958."Includes bibliographical references (p. 7).Mode of access: Internet

Experimental pressure distributions on a blunt lifting-entry body at Mach 3.71 /

Morris, W. Douglas.
Couch, Lana M.
Langley Research Center.
United States. National Aeronautics and Space Administration.

January 1968

Cover title."April 1968."Includes bibliographical references (p. 12).Mode of access: Internet

Research on blunt-faced entry configurations at angles of attack Between 60° and 90° /

Phillips, William H.
Langley Research Center.

January 1960

"September 1960."Cover title.Includes bibliographical references (p. 9).Mode of access: Internet

Supersonic aerodynamics of large-angle cones /

Campbell, James F.
Howell, Dorothy T.
Langley Research Center.
United States. National Aeronautics and Space Administration.

January 1968

Cover title."August 1968."Includes bibliographical references (p. 13).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

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...

Experimental investigation of the transonic flutter of simple thin truncated-cone panels /

Gilman, Jean.
Langley Research Center.

January 1961

"October 1961."Cover title.Includes bibliographical references (p. 13).Mode of access: Internet

Design guide for pitch-up evaluation and investigation at high subsonic speeds of possible limitations due to wing-aspect-ratio variations /

Spreemann, Kenneth P.
United States. National Aeronautics and Space Administration.

"August 1959."Cover title.Includes bibliographical references (p. 14-16).Mode of access: Internet

Experimental investigation of a disk-shaped reentry configuration at transonic and low supersonic speeds /

Lazzeroni, Frank A.
United States. National Aeronautics and Space Administration.

"May 1962."Cover title.Includes bibliographical references (p. 7).Mode of access: Internet

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

Investigation of the low-subsonic stability and control characteristics of a 0.34-scale free-flying model of a modified half-cone reentry vehicle /

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

"January 1962."Cover title.Includes bibliographical references (p. 15).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

Aerodynamic characteristics of a modified cone : conical-frustum entry configuration at Mach 6.0 /

Ashby, George C.
Staylor, W. Frank.
Langley Research Center.
United States. National Aeronautics and Space Administration.

January 1968

Cover title."June 1968."Includes bibliographical references (p. 8).Mode of access: Internet

Subsonic aerodynamic characteristics of disk re-entry configurations with elliptic cross sections and thickness-diameter ratios of 0.225 and 0.325 /

Demele, Fred A.
Brownson, Jack J.
United States. National Aeronautics and Space Administration.

"May 1961."Cover title.Includes bibliographical references (p. 9-10).Mode of access: Internet

Investigation of a retrorocket exhausting from the nose of a blunt body into a supersonic free stream /

Charczenko, Nickolai.
Hennessey, Katherine W.
United States. National Aeronautics and Space Administration.

Cover title."September 1961."Aerodynamics, missiles and space vehicles; Atmospheric entry.Includes b...

Investigation of an underslung half-cone inlet with compression surface mounted outboard from fuselage at mach numbers of 1.5, 1.8, and 2.0 /

Yeager, Richard A.
Gertsma, Laurence W.
Lewis Flight Propulsion Laboratory.
United States. National Adviosry Committee for Aeronautics. NACA research memorandum.

January 1958

"May 12, 1958."Includes bibliographical references (p. 7).Mode of access: Internet

Experimental pressure distributions on a blunt lifting-entry body at Mach 3.71 /

Morris, W. Douglas.
Couch, Lana M.
Langley Research Center.
United States. National Aeronautics and Space Administration.

January 1968

Cover title."April 1968."Includes bibliographical references (p. 12).Mode of access: Internet

Research on blunt-faced entry configurations at angles of attack Between 60° and 90° /

Phillips, William H.
Langley Research Center.

January 1960

"September 1960."Cover title.Includes bibliographical references (p. 9).Mode of access: Internet

Supersonic aerodynamics of large-angle cones /

Campbell, James F.
Howell, Dorothy T.
Langley Research Center.
United States. National Aeronautics and Space Administration.

January 1968

Cover title."August 1968."Includes bibliographical references (p. 13).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

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...

Experimental investigation of the transonic flutter of simple thin truncated-cone panels /

Gilman, Jean.
Langley Research Center.

January 1961

"October 1961."Cover title.Includes bibliographical references (p. 13).Mode of access: Internet

Design guide for pitch-up evaluation and investigation at high subsonic speeds of possible limitations due to wing-aspect-ratio variations /

Spreemann, Kenneth P.
United States. National Aeronautics and Space Administration.

"August 1959."Cover title.Includes bibliographical references (p. 14-16).Mode of access: Internet

A preliminary investigation of modified blunt 13° half-cone re-entry configurations at subsonic speeds /

Abstract

Extracted data

A preliminary investigation of modified blunt 13° half-cone re-entry configurations at subsonic speeds /

Abstract

Extracted data

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