Drag coefficients for spheres in free molecular flow in O at satellite velocities /

An experimental investigation of a cold jet emitting from a body of revolution into a subsonic free stream /

Ousterhout, Donald Stewart, 1929-
Langley Research Center.
Old Dominion University. Research Foundation.

January 1972

"Prepared by Old Dominion University Research Foundation ... for Langley Research Center."Cover titl...

Theoretical and experimental study of a new method for prediction of profile drag of airfoil sections /

Goradia, Suresh H. (Suresh Harkisondas), 1937-
Lilley, D. G.
Langley Research Center.
Lockheed-Georgia Company.

"Prepared by Lockheed-Georgia Company ... for Langley Research Center.""June 1975."Cover title.Inclu...

Drag of a supercritical body of revolution in free flight at transonic speeds and comparison with wind-tunnel data /

Usry, J. W.
Wallace, John W.
Langley Research Center.
United States. National Aeronautics and Space Administration.

January 1971

Prepared at Langley Research Center."December 1971."Includes bibliographical references (p. 13).Mode...

Determination of the hypersonic-continuum/rarefield-flow drag coefficient of the Viking Lander Capsule 1 aeroshell from flight data /

Blanchard, Robert C.
Walberg, Gerald D.
Langley Research Center.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.

January 1980

Dec. 1980."Langley Research Center."Includes bibliographical references.Mode of access: Internet

Study of lee-side flows over conically cambered delta wings at supersonic speeds /

Wood, Richard M.
Watson, Carolyn B.
Langley Research Center.

January 1987

Prepared at Langley Research Center.Bibliography: v. 1, p. 26.Mode of access: Internet

Drag coefficients for spheres in free molecular flow in O at satellite velocities

Humphris, R. R.
Boring, J. W.

March 1973

The drag coefficients for the Echo 1 and Explorer 24 spherical surfaces in an O environment were exp...

The orbital mechanics of flight mechanics.

Dunning, Robert Scott.
Langley Research Center.

January 1973

"Prepared by NASA Langley Research Center."Bibliography: p. 146-149.Mode of access: Internet

Jet effects on the drag of conical afterbodies at spersonic speeds /

Compton, William B.
Langley Research Center.

January 1972

Prepared at Langley Research Center.Cover title.Bibliography: p. 13.Mode of access: Internet

Boundary layer stability on a yawed spinning body of revolution and its effect on the magnus force and moment /

Jacobson, I. D. (Ira D.)
Morton, J. B.
Langley Research Center.
University of Virginia.

January 1972

"Prepared by University of Virginia ... for Langley Research Center."Cover title.Bibliography: p. 34...

Semianalytic modeling of aerodynamic shapes /

Barger, Raymond L.
Adams, Mary S.
Langley Research Center.

January 1985

Prepared at Langley Research Center."April 1985"--Cover.Includes bibliographical references (p. 6).M...

Aerodynamic characteristics of an oblate spheroid and a sphere at Mach numbers from 1.70 to 10.49 /

Jernell, Lloyd S.
Langley Research Center.
United States. National Aeronautics and Space Administration.

January 1970

Drag coefficients of oblate spheroid and sphere at Mach numbers from 1.70 to 10.49.Includes bibliogr...

Importance of the variation of drag with lift in minimization of satellite entry acceleration /

Grant, Frederick C.
Langley Research Center.

January 1959

"NASA TN D-120.""Langley Research Center, Langley Field, Va.""October 1959."Title from cover.Include...

The Aerodynamics of bodies in a rarefied ionized gas with applications to spacecraft environmental dynamics /

Stone, Nobie H.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.
George C. Marshall Space Flight Center.

January 1981

"November 1981"--Cover."George C. Marshall Space Flight Center."Includes bibliographical references....

Aerodynamic characteristics of a large aircraft to transport space shuttle orbiter or other external payloads /

Paulson, John W.
Langley Research Center.

January 1975

Prepared at Langley Research Center.Cover title.Includes bibliographical references (p. 12).Mode of ...

Wind tunnel simulation of full scale vortices /

Rorke, James B.
Moffitt, Robert C.
Langley Research Center.
United Aircraft Corporation. Sikorsky Aircraft Division.

January 1973

"Prepared by Sikorsky Aircraft Division, United Aircraft Corporation ... for Langley Research Center...

An experimental investigation of a cold jet emitting from a body of revolution into a subsonic free stream /

Ousterhout, Donald Stewart, 1929-
Langley Research Center.
Old Dominion University. Research Foundation.

January 1972

"Prepared by Old Dominion University Research Foundation ... for Langley Research Center."Cover titl...

Theoretical and experimental study of a new method for prediction of profile drag of airfoil sections /

Goradia, Suresh H. (Suresh Harkisondas), 1937-
Lilley, D. G.
Langley Research Center.
Lockheed-Georgia Company.

"Prepared by Lockheed-Georgia Company ... for Langley Research Center.""June 1975."Cover title.Inclu...

Drag of a supercritical body of revolution in free flight at transonic speeds and comparison with wind-tunnel data /

Usry, J. W.
Wallace, John W.
Langley Research Center.
United States. National Aeronautics and Space Administration.

January 1971

Prepared at Langley Research Center."December 1971."Includes bibliographical references (p. 13).Mode...

Determination of the hypersonic-continuum/rarefield-flow drag coefficient of the Viking Lander Capsule 1 aeroshell from flight data /

Blanchard, Robert C.
Walberg, Gerald D.
Langley Research Center.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.

January 1980

Dec. 1980."Langley Research Center."Includes bibliographical references.Mode of access: Internet

Study of lee-side flows over conically cambered delta wings at supersonic speeds /

Wood, Richard M.
Watson, Carolyn B.
Langley Research Center.

January 1987

Prepared at Langley Research Center.Bibliography: v. 1, p. 26.Mode of access: Internet

Drag coefficients for spheres in free molecular flow in O at satellite velocities

Humphris, R. R.
Boring, J. W.

March 1973

The drag coefficients for the Echo 1 and Explorer 24 spherical surfaces in an O environment were exp...

The orbital mechanics of flight mechanics.

Dunning, Robert Scott.
Langley Research Center.

January 1973

"Prepared by NASA Langley Research Center."Bibliography: p. 146-149.Mode of access: Internet

Jet effects on the drag of conical afterbodies at spersonic speeds /

Compton, William B.
Langley Research Center.

January 1972

Prepared at Langley Research Center.Cover title.Bibliography: p. 13.Mode of access: Internet

Boundary layer stability on a yawed spinning body of revolution and its effect on the magnus force and moment /

Jacobson, I. D. (Ira D.)
Morton, J. B.
Langley Research Center.
University of Virginia.

January 1972

"Prepared by University of Virginia ... for Langley Research Center."Cover title.Bibliography: p. 34...

Semianalytic modeling of aerodynamic shapes /

Barger, Raymond L.
Adams, Mary S.
Langley Research Center.

January 1985

Prepared at Langley Research Center."April 1985"--Cover.Includes bibliographical references (p. 6).M...

Aerodynamic characteristics of an oblate spheroid and a sphere at Mach numbers from 1.70 to 10.49 /

Jernell, Lloyd S.
Langley Research Center.
United States. National Aeronautics and Space Administration.

January 1970

Drag coefficients of oblate spheroid and sphere at Mach numbers from 1.70 to 10.49.Includes bibliogr...

Importance of the variation of drag with lift in minimization of satellite entry acceleration /

Grant, Frederick C.
Langley Research Center.

January 1959

"NASA TN D-120.""Langley Research Center, Langley Field, Va.""October 1959."Title from cover.Include...

The Aerodynamics of bodies in a rarefied ionized gas with applications to spacecraft environmental dynamics /

Stone, Nobie H.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.
George C. Marshall Space Flight Center.

January 1981

"November 1981"--Cover."George C. Marshall Space Flight Center."Includes bibliographical references....

Aerodynamic characteristics of a large aircraft to transport space shuttle orbiter or other external payloads /

Paulson, John W.
Langley Research Center.

January 1975

Prepared at Langley Research Center.Cover title.Includes bibliographical references (p. 12).Mode of ...

Wind tunnel simulation of full scale vortices /

Rorke, James B.
Moffitt, Robert C.
Langley Research Center.
United Aircraft Corporation. Sikorsky Aircraft Division.

January 1973

"Prepared by Sikorsky Aircraft Division, United Aircraft Corporation ... for Langley Research Center...

An experimental investigation of a cold jet emitting from a body of revolution into a subsonic free stream /

Ousterhout, Donald Stewart, 1929-
Langley Research Center.
Old Dominion University. Research Foundation.

January 1972

"Prepared by Old Dominion University Research Foundation ... for Langley Research Center."Cover titl...

Theoretical and experimental study of a new method for prediction of profile drag of airfoil sections /

Goradia, Suresh H. (Suresh Harkisondas), 1937-
Lilley, D. G.
Langley Research Center.
Lockheed-Georgia Company.

"Prepared by Lockheed-Georgia Company ... for Langley Research Center.""June 1975."Cover title.Inclu...

Drag of a supercritical body of revolution in free flight at transonic speeds and comparison with wind-tunnel data /

Usry, J. W.
Wallace, John W.
Langley Research Center.
United States. National Aeronautics and Space Administration.

January 1971

Prepared at Langley Research Center."December 1971."Includes bibliographical references (p. 13).Mode...

Drag coefficients for spheres in free molecular flow in O at satellite velocities /

Abstract

Extracted data

Drag coefficients for spheres in free molecular flow in O at satellite velocities /

Abstract

Extracted data

Related items

Related items