Wind-tunnel investigation of the static and dynamic stability characteristics of a 10 degree semivertex angle blunted cone /

Transonic investigation of the effects of nose bluntness, fineness ratio, cone angle, and base shape on the static aerodynamic characteristics of short, blunt cones at angles of attack to 180⁰ /

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

Cover title."August 1963."Includes bibliographical references.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

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...

Static aerodynamic characteristics of short blunt cones with various nose and base cone angles at Mach numbers from 0.6 to 5.5 and angles of attack to 180 degrees /

Treon, Stuart L.
United States. National Aeronautics and Space Administration.

Cover title."May 1962."Aerodynamics, missiles and space vehicles; Fluid mechanics; Space vehicles; S...

Free-flight measurements of the static and dynamic stability and drag of a 10 degree blunted cone at mach numbers 3.5 and 8.5 Peter F. Intrieri.

Intrieri, Peter F.
United States. National Aeronautics and Space Administration.

Cover title."May 1962."Aerodynamics, missiles and space vehicles; Atmospheric entry; Fluid mechanics...

Motions of a short 10 degree blunted cone entering a Martian atmosphere at arbitrary angles of attack and arbitrary pitching rates /

Peterson, Victor L.
United States. National Aeronautics and Space Administration.

Cover title."May 1962."Aerodynamics, missiles and space vehicles; Atmospheric entry; Fluid mechanics...

Wind-tunnel investigation of a small-scale model of an aerial vehicle supported by tilting ducted fans /

Smith, Charles C.
United States. National Aeronautics and Space Administration.

Cover title."August 1960."Aerodynamics, aircraft; Stability and control.Includes bibliographical ref...

Pressure measurements on sharp and blunt 5 degreee and 15 degree-half-angle cones at mach number 3.86 and angles of attack to 100 degrees /

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

Cover title."February 1961."Aerodynamics, missiles and space vehicles; Fluid mechanics.Includes bibl...

Drag characteristics and dynamic stability in descent of a rotary parachute tested in a vertical tunnel /

Burk, Sanger M.
United States. National Aeronautics and Space Administration.

Cover title."August 1962."Aerodynamics, missiles and space vehicles; Atmospheric entry.Includes bibl...

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

Aerodynamic characteristics of towed cones used as decelerators at mach numbers rom 1.57 to 4.65 /

Charczenko, Nickolai.
McShera, John T.
United States. National Aeronautics and Space Administration.

Cover title." December 1961."Aerodynamics, missiles and space vehicles;Atmospheric entry.Includes bi...

Wind-tunnel tests of a series of 18-foot-diameter parachutes with extendable flaps /

Gamse, Berl.
Yaggy, Paul F.
United States. National Aeronautics and Space Administration.

Cover title."August 1962."Aerodynamics, missiles and space vehicles; Atmospheric entry.Includes bibl...

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

Analytical and experimental investigation of flutter and divergence of speed-mounted cone configurations at supersonic speeds / y John L. Sewall, Robert W. Hess and Charles E. Watkins.

Sewall, John L.
Watkins, Charles E.
Hess, Robert W.
United States. National Aeronautics and Space Administration.

Cover title."April 1962."Aerodynamics, missiles and space vehicles; Fluid mechanics; Stresses and lo...

Design and calibration of an arc-heated, hypersonic, low-density wind tunnel

Weitmann, Ruth N.
United States. National Aeronautics and Space Administration.

Cover title."August 1962."Aerodynamics, missiles and space vehicles; Atmospheric entry; Chemistry, p...

Transonic investigation of the effects of nose bluntness, fineness ratio, cone angle, and base shape on the static aerodynamic characteristics of short, blunt cones at angles of attack to 180⁰ /

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

Cover title."August 1963."Includes bibliographical references.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

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...

Static aerodynamic characteristics of short blunt cones with various nose and base cone angles at Mach numbers from 0.6 to 5.5 and angles of attack to 180 degrees /

Treon, Stuart L.
United States. National Aeronautics and Space Administration.

Cover title."May 1962."Aerodynamics, missiles and space vehicles; Fluid mechanics; Space vehicles; S...

Free-flight measurements of the static and dynamic stability and drag of a 10 degree blunted cone at mach numbers 3.5 and 8.5 Peter F. Intrieri.

Intrieri, Peter F.
United States. National Aeronautics and Space Administration.

Cover title."May 1962."Aerodynamics, missiles and space vehicles; Atmospheric entry; Fluid mechanics...

Motions of a short 10 degree blunted cone entering a Martian atmosphere at arbitrary angles of attack and arbitrary pitching rates /

Peterson, Victor L.
United States. National Aeronautics and Space Administration.

Cover title."May 1962."Aerodynamics, missiles and space vehicles; Atmospheric entry; Fluid mechanics...

Wind-tunnel investigation of a small-scale model of an aerial vehicle supported by tilting ducted fans /

Smith, Charles C.
United States. National Aeronautics and Space Administration.

Cover title."August 1960."Aerodynamics, aircraft; Stability and control.Includes bibliographical ref...

Pressure measurements on sharp and blunt 5 degreee and 15 degree-half-angle cones at mach number 3.86 and angles of attack to 100 degrees /

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

Cover title."February 1961."Aerodynamics, missiles and space vehicles; Fluid mechanics.Includes bibl...

Drag characteristics and dynamic stability in descent of a rotary parachute tested in a vertical tunnel /

Burk, Sanger M.
United States. National Aeronautics and Space Administration.

Cover title."August 1962."Aerodynamics, missiles and space vehicles; Atmospheric entry.Includes bibl...

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

Aerodynamic characteristics of towed cones used as decelerators at mach numbers rom 1.57 to 4.65 /

Charczenko, Nickolai.
McShera, John T.
United States. National Aeronautics and Space Administration.

Cover title." December 1961."Aerodynamics, missiles and space vehicles;Atmospheric entry.Includes bi...

Wind-tunnel tests of a series of 18-foot-diameter parachutes with extendable flaps /

Gamse, Berl.
Yaggy, Paul F.
United States. National Aeronautics and Space Administration.

Cover title."August 1962."Aerodynamics, missiles and space vehicles; Atmospheric entry.Includes bibl...

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

Analytical and experimental investigation of flutter and divergence of speed-mounted cone configurations at supersonic speeds / y John L. Sewall, Robert W. Hess and Charles E. Watkins.

Sewall, John L.
Watkins, Charles E.
Hess, Robert W.
United States. National Aeronautics and Space Administration.

Cover title."April 1962."Aerodynamics, missiles and space vehicles; Fluid mechanics; Stresses and lo...

Design and calibration of an arc-heated, hypersonic, low-density wind tunnel

Weitmann, Ruth N.
United States. National Aeronautics and Space Administration.

Cover title."August 1962."Aerodynamics, missiles and space vehicles; Atmospheric entry; Chemistry, p...

Transonic investigation of the effects of nose bluntness, fineness ratio, cone angle, and base shape on the static aerodynamic characteristics of short, blunt cones at angles of attack to 180⁰ /

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

Cover title."August 1963."Includes bibliographical references.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

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 static and dynamic stability characteristics of a 10 degree semivertex angle blunted cone /

Abstract

Extracted data

Wind-tunnel investigation of the static and dynamic stability characteristics of a 10 degree semivertex angle blunted cone /

Abstract

Extracted data

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