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

Flight and wind-tunnel measurements showing base drag reduction provided by a trailing disk for high Reynolds number turbulent flow for subsonic and transonic Mach numbers /

Powers, Sheryll Goecke.
Fox, Charles H.
Huffman, Jarrett K.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.

January 1986

Includes bibliographical references (p. 22-23)."November 1986"--Cover.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 (...

Flight tests of Viking parachute system in three Mach number regimes /

Lundstrom, Reginald R.
Langley Research Center.

January 1974

Prepared at Langley Research Center.Cover title.Includes bibliographical references.1. Vehicle descr...

Determination of the hypersonic-continuum/rarefied-flow drag coefficient of the Viking lander capsule 1 aeroshell from flight data

Blanchard, R. C.
Walberg, G. D.

December 1980

Results of an investigation to determine the full scale drag coefficient in the high speed, low dens...

Investigation of the aerodynamic characteristics of a hypersonic transport model at Mach numbers to 6 /

Ellison, James C.
United States. National Aeronautics and Space Administration.
Langley Research Center.

January 1971

Also available online.Prepared at the Langley Research Center.N71-23127.Includes bibliographical ref...

Experimental and theoretical aerodynamic characteristics of two hypersonic cruise aircraft concepts at Mach numbers of 2.96, 3.96, and 4.63 /

Pittman, Jimmy L.
Riebe, Gregory 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

Drag measurements of blunt stores tangentially mounted on a flat plate at supersonic speeds /

Wilcox, Floyd J. (Floyd Jay)
Langley Research Center.

January 1987

Prepared at Langley Research Center."September 1987"--Cover.Includes bibliographical references (p. ...

Viking entry vehicle aerodynamics at M = 2 in air and some preliminary test data for flight in CO₂ at M = 11 /

Sammonds, Robert I.
Kruse, Robert L. (Robert Leroy), 1941-
Ames Research Center.

January 1975

Prepared at Ames Research Center.Cover title.Includes bibliographical references (p. 7).Mode of acce...

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

Boring, John W.
Humphris, Robert R.
Langley Research Center.
University of Virginia.

January 1973

"Prepared by University of Virginia ... for Langley Research Center."Cover title.Bibliography: p. 35...

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...

Exploratory investigation of the aerodynamic characteristics of a biwing vehicle at Mach 20.3 /

Bernot, Peter T.
Langley Research Center.

January 1985

Prepared at Langley Research Center."February 1985"--Cover.Includes bibliographical references (p. 4...

Experimental determination of aerodynamic drag on a blunted 10-deg cone at angles of attack in hypersonic, rarefied flow /

Boylan, David E., author.
Sims, William H., author.
ARO, Inc., sponsor.
Arnold Engineering Development Center. sponsor.
United States. Air Force. Systems Command. issuing body.

Report prepared by ARO, Inc., a subsidiary of Sverdrup and Parcel, Inc."April 1964."Includes bibliog...

Experimental investigation at Mach 8 of the effects of projections and cavities on heat transfer to a model of the Viking aeroshell /

Creel, Theodore R.
Langley Research Center.

January 1974

Prepared at Langley Research Center.Cover title.Includes bibliographical references (p. 7).Mode of a...

A free-flight investigation of the drag coefficients of two single-engine supersonic interceptor configurations from Mach number 0.8 to 1.90 to determine the effect of inlet and engine locations /

Judd, Joseph H.
Langley Aeronautical Laboratory.
United States. National Adviosry Committee for Aeronautics. NACA research memorandum.

January 1955

"September 28, 1955."Includes bibliographical references (p. 14-15).Mode of access: Internet

Viking Mars mission support investigations in the Langley Transonic Dynamics Tunnel /

Foughner, Jerome T.
Langley Research Center.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Office.

January 1980

"May 1980"--Cover."Langley Research Center."Includes bibliographical references.Mode of access: Inte...

Flight and wind-tunnel measurements showing base drag reduction provided by a trailing disk for high Reynolds number turbulent flow for subsonic and transonic Mach numbers /

Powers, Sheryll Goecke.
Fox, Charles H.
Huffman, Jarrett K.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.

January 1986

Includes bibliographical references (p. 22-23)."November 1986"--Cover.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 (...

Flight tests of Viking parachute system in three Mach number regimes /

Lundstrom, Reginald R.
Langley Research Center.

January 1974

Prepared at Langley Research Center.Cover title.Includes bibliographical references.1. Vehicle descr...

Determination of the hypersonic-continuum/rarefied-flow drag coefficient of the Viking lander capsule 1 aeroshell from flight data

Blanchard, R. C.
Walberg, G. D.

December 1980

Results of an investigation to determine the full scale drag coefficient in the high speed, low dens...

Investigation of the aerodynamic characteristics of a hypersonic transport model at Mach numbers to 6 /

Ellison, James C.
United States. National Aeronautics and Space Administration.
Langley Research Center.

January 1971

Also available online.Prepared at the Langley Research Center.N71-23127.Includes bibliographical ref...

Experimental and theoretical aerodynamic characteristics of two hypersonic cruise aircraft concepts at Mach numbers of 2.96, 3.96, and 4.63 /

Pittman, Jimmy L.
Riebe, Gregory 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

Drag measurements of blunt stores tangentially mounted on a flat plate at supersonic speeds /

Wilcox, Floyd J. (Floyd Jay)
Langley Research Center.

January 1987

Prepared at Langley Research Center."September 1987"--Cover.Includes bibliographical references (p. ...

Viking entry vehicle aerodynamics at M = 2 in air and some preliminary test data for flight in CO₂ at M = 11 /

Sammonds, Robert I.
Kruse, Robert L. (Robert Leroy), 1941-
Ames Research Center.

January 1975

Prepared at Ames Research Center.Cover title.Includes bibliographical references (p. 7).Mode of acce...

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

Boring, John W.
Humphris, Robert R.
Langley Research Center.
University of Virginia.

January 1973

"Prepared by University of Virginia ... for Langley Research Center."Cover title.Bibliography: p. 35...

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...

Exploratory investigation of the aerodynamic characteristics of a biwing vehicle at Mach 20.3 /

Bernot, Peter T.
Langley Research Center.

January 1985

Prepared at Langley Research Center."February 1985"--Cover.Includes bibliographical references (p. 4...

Experimental determination of aerodynamic drag on a blunted 10-deg cone at angles of attack in hypersonic, rarefied flow /

Boylan, David E., author.
Sims, William H., author.
ARO, Inc., sponsor.
Arnold Engineering Development Center. sponsor.
United States. Air Force. Systems Command. issuing body.

Report prepared by ARO, Inc., a subsidiary of Sverdrup and Parcel, Inc."April 1964."Includes bibliog...

Experimental investigation at Mach 8 of the effects of projections and cavities on heat transfer to a model of the Viking aeroshell /

Creel, Theodore R.
Langley Research Center.

January 1974

Prepared at Langley Research Center.Cover title.Includes bibliographical references (p. 7).Mode of a...

A free-flight investigation of the drag coefficients of two single-engine supersonic interceptor configurations from Mach number 0.8 to 1.90 to determine the effect of inlet and engine locations /

Judd, Joseph H.
Langley Aeronautical Laboratory.
United States. National Adviosry Committee for Aeronautics. NACA research memorandum.

January 1955

"September 28, 1955."Includes bibliographical references (p. 14-15).Mode of access: Internet

Viking Mars mission support investigations in the Langley Transonic Dynamics Tunnel /

Foughner, Jerome T.
Langley Research Center.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Office.

January 1980

"May 1980"--Cover."Langley Research Center."Includes bibliographical references.Mode of access: Inte...

Flight and wind-tunnel measurements showing base drag reduction provided by a trailing disk for high Reynolds number turbulent flow for subsonic and transonic Mach numbers /

Powers, Sheryll Goecke.
Fox, Charles H.
Huffman, Jarrett K.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.

January 1986

Includes bibliographical references (p. 22-23)."November 1986"--Cover.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 (...

Flight tests of Viking parachute system in three Mach number regimes /

Lundstrom, Reginald R.
Langley Research Center.

January 1974

Prepared at Langley Research Center.Cover title.Includes bibliographical references.1. Vehicle descr...

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

Abstract

Extracted data

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

Abstract

Extracted data

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