Aerodynamic heating of conical entry vehicles at speeds in excess of earth parabolic speed /

Atmosphere entries with vehicle lift-drag ration modulated to limit deceleration and rate of deceleration: vehicles with maximum lift-drag ration of 0.5 /

Katzen, Elliott D.
Levy, Lionel L.
United States. National Aeronautics and Space Administration.

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

External-drag estimation for slender conical ducted bodies at high mach numbers and zero angle of attack. /

Valentine, E. Floyd
United States. National Aeronautics and Space Administration.

Cover title."March 1961."Aerodynamics, aircraft; Aircraft.Includes bibliographical references.Mode o...

Aerodynamic heating and heat transfer phenomena at Mach numbers 3 to 4 /

Anderson, K. G., author.
Durben, J. M., author.
Merrell, H. B., author.
Wright Air Development Center. issuing body.
United States. Air Force. Air Research and Development Command. sponsor.

"December 1951."Includes bibliographical references (pages 45-47).Aero Medical Laboratory Contract N...

One-dimensional heat conduction through the skin of a vehicle upon entering a planetary atmosphere at constant velocity and entry angle /

Wells, William R.
McLellan, Charles H.
United States. National Aeronautics and Space Administration.

Cover title."October 1962."Aerodynamics, missiles and space vehicles; Atmospheric entry; Fluid mecha...

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

Aerodynamic heating and loading within large open cavities in cone and cone-cyclinder-flare models at Mach 6.7 /

Hunt, L. Roane (Lewis Roane)
Langley Research Center.

January 1974

Prepared at Langley Research Center.Cover title.Includes bibliographical references (p. 13).Mode of ...

Aerodynamic heating of conical entry vehicles at speeds in excess of earth parabolic speed

Winovich, W.
Allen, H. J.
Seiff, A.

December 1963

Aerodynamic heating of conical vehicles entering earth atmosphere at speeds greater than earth parab...

Heat transfer to blunt nose shapes with laminar boundary layers at high supersonic speeds /

Reller, John O. Jr.
United States. National Advisory Committee for Aeronautics. NACA research memorandum.
Ames Research Center.

On front cover: "August 16, 1957."Includes bibliographical references: p. 6-7.Mode of access: Intern...

Convective heat transfer to a lifting flat-faced-cone entry body /

Terry, James E.
Ames Research Center.

January 1961

"May 1961."Cover title.Includes bibliographical references (p. 18-19).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...

Aerodynamic pressures and heating rates on surfaces between split elevons at Mach 6.6 /

Hunt, L. Roane (Lewis Roane)
United States. National Aeronautics and Space Administration. Scientific and Technical Information Division.

January 1988

"December 1988"--Cover.Includes bibliographical references (p. 13).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

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...

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

Aerodynamic-heating data obtained from free-flight tests between Mach numbers of 1 and 5 /

Rumsey, Charles B. (Charles Bertrand)
Hopko, Russell N.
Piland, Robert Owens.
Langley Research Center.

Prepared at Langley Research Center."January 1960."Cover title.Includes bibliographical references (...

Atmosphere entries with vehicle lift-drag ration modulated to limit deceleration and rate of deceleration: vehicles with maximum lift-drag ration of 0.5 /

Katzen, Elliott D.
Levy, Lionel L.
United States. National Aeronautics and Space Administration.

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

External-drag estimation for slender conical ducted bodies at high mach numbers and zero angle of attack. /

Valentine, E. Floyd
United States. National Aeronautics and Space Administration.

Cover title."March 1961."Aerodynamics, aircraft; Aircraft.Includes bibliographical references.Mode o...

Aerodynamic heating and heat transfer phenomena at Mach numbers 3 to 4 /

Anderson, K. G., author.
Durben, J. M., author.
Merrell, H. B., author.
Wright Air Development Center. issuing body.
United States. Air Force. Air Research and Development Command. sponsor.

"December 1951."Includes bibliographical references (pages 45-47).Aero Medical Laboratory Contract N...

One-dimensional heat conduction through the skin of a vehicle upon entering a planetary atmosphere at constant velocity and entry angle /

Wells, William R.
McLellan, Charles H.
United States. National Aeronautics and Space Administration.

Cover title."October 1962."Aerodynamics, missiles and space vehicles; Atmospheric entry; Fluid mecha...

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

Aerodynamic heating and loading within large open cavities in cone and cone-cyclinder-flare models at Mach 6.7 /

Hunt, L. Roane (Lewis Roane)
Langley Research Center.

January 1974

Prepared at Langley Research Center.Cover title.Includes bibliographical references (p. 13).Mode of ...

Aerodynamic heating of conical entry vehicles at speeds in excess of earth parabolic speed

Winovich, W.
Allen, H. J.
Seiff, A.

December 1963

Aerodynamic heating of conical vehicles entering earth atmosphere at speeds greater than earth parab...

Heat transfer to blunt nose shapes with laminar boundary layers at high supersonic speeds /

Reller, John O. Jr.
United States. National Advisory Committee for Aeronautics. NACA research memorandum.
Ames Research Center.

On front cover: "August 16, 1957."Includes bibliographical references: p. 6-7.Mode of access: Intern...

Convective heat transfer to a lifting flat-faced-cone entry body /

Terry, James E.
Ames Research Center.

January 1961

"May 1961."Cover title.Includes bibliographical references (p. 18-19).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...

Aerodynamic pressures and heating rates on surfaces between split elevons at Mach 6.6 /

Hunt, L. Roane (Lewis Roane)
United States. National Aeronautics and Space Administration. Scientific and Technical Information Division.

January 1988

"December 1988"--Cover.Includes bibliographical references (p. 13).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

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...

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

Aerodynamic-heating data obtained from free-flight tests between Mach numbers of 1 and 5 /

Rumsey, Charles B. (Charles Bertrand)
Hopko, Russell N.
Piland, Robert Owens.
Langley Research Center.

Prepared at Langley Research Center."January 1960."Cover title.Includes bibliographical references (...

Atmosphere entries with vehicle lift-drag ration modulated to limit deceleration and rate of deceleration: vehicles with maximum lift-drag ration of 0.5 /

Katzen, Elliott D.
Levy, Lionel L.
United States. National Aeronautics and Space Administration.

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

External-drag estimation for slender conical ducted bodies at high mach numbers and zero angle of attack. /

Valentine, E. Floyd
United States. National Aeronautics and Space Administration.

Cover title."March 1961."Aerodynamics, aircraft; Aircraft.Includes bibliographical references.Mode o...

Aerodynamic heating and heat transfer phenomena at Mach numbers 3 to 4 /

Anderson, K. G., author.
Durben, J. M., author.
Merrell, H. B., author.
Wright Air Development Center. issuing body.
United States. Air Force. Air Research and Development Command. sponsor.

"December 1951."Includes bibliographical references (pages 45-47).Aero Medical Laboratory Contract N...

Aerodynamic heating of conical entry vehicles at speeds in excess of earth parabolic speed /

Abstract

Extracted data

Aerodynamic heating of conical entry vehicles at speeds in excess of earth parabolic speed /

Abstract

Extracted data

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