Some aspects of air-helium simulation and hypersonic approximations /

Loads induced on a flat plate at a Mach number of 4.5 with a sonic or supersonic jet exhausting normal to the surface /

Letko, William.
Langley Research Center.

Prepared at Langley Research Center."July 1963."Cover title.Includes bibliographical references (p. ...

An exploratory simulation study of a head-on display for general aviation lightplanes /

Harris, Randall L.
Hewes, Donald E.
Langley Research Center.

January 1973

Prepared at Langley Research Center.Cover title.Includes bibliographical references (p. 27).Mode of ...

A rendezvous and station-keeping simulator with fly-around capability and virtual-image viewing /

Kahlbaum, William M.
Stumpf, John J.
Bardusch, Richard E.
United States. National Aeronautics and Space Administration.
Langley Research Center.

Prepared at Langley Research Center."April 1969"--Cover.Includes bibliographical references (p. 20)....

Air-helium simulation of the aerodynamic force coefficients of cones at hypersonic speeds /

Ladson, Charles L.
Blackstock, Thomas A.
United States. National Aeronautics and Space Administration.

Cover title."October 1962."Aerodynamics, missiles and space vehicles; Fluid mechanics; Simulators an...

Description of a 2-foot hypersonic facility at the Langley Research Center /

Stokes, George M.
Langley Research Center.

Prepared at Langley Research Center."September 1961."Cover title.Includes bibliographical references...

Effect of air contamination in a helium tunnel /

Henderson, Arthur, 1922-
Swalley, Frank E. (Frank Edwin), 1936-
Langley Research Center.

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

Ideal-gas tables for helium flow in the Mach number range from 40 to 100 /

Mueller, James N.
Langley Research Center.

Prepared at Langley Research Center."May 1962."Cover title.Includes bibliographical references (p. 6...

Transition fixing for hypersonic flow /

Sterrett, James R.
Langley Research Center.

Prepared at Langley Research Center."October 1967"--Cover.Includes bibliographical references (p. 12...

A simulation investigation of the loads experienced by a piloted launch vehicle /

Sleeper, Robert K.
Langley Research Center.

Prepared at Langley Research Center."March 1966"--Cover.Includes bibliographical references (p. 33)....

A study of equilibrium real-gas effects in hypersonic air nozzles, including charts of thermodynamic properties for equilibrium air /

Erickson, Wayne D. (Wayne Douglas), 1932-
Creekmore, Helen S.
Langley Research Center.

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

Aerodynamic testing technique for twin-fuselage models at hypersonic speeds /

Ashby, George C.
Langley Research Center.

January 1975

Prepared at Langley Research Center.Cover title.Includes bibliographical references (p. 6).Mode of a...

Structural concepts for hydrogen-fueled hypersonic airplanes /

Jackson, L. Robert.
Wichorek, Gregory R.
Davis, John G.
United States. National Aeronautics and Space Administration.
Langley Research Center.

"February 1966"--Cover.Includes bibliographical references.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 (...

Operating characteristics of the Langley Mach 10 high Reynolds number helium tunnel /

Watson, Ralph D.
Fischer, Michael C.
Morris, Dana J.
Langley Research Center.

January 1974

Prepared at Langley Research Center.Cover title.Includes bibliographical references (p. 10).Mode of ...

Fixed-base simulation study of a pilot's ability to control a winged-satellite vehicle during high-drag variable-lift entries /

Eggleston, John M. (John Marshall)
Cheatham, Donald C.
Baron, Sheldon.
Langley Research Center.

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

Loads induced on a flat plate at a Mach number of 4.5 with a sonic or supersonic jet exhausting normal to the surface /

Letko, William.
Langley Research Center.

Prepared at Langley Research Center."July 1963."Cover title.Includes bibliographical references (p. ...

An exploratory simulation study of a head-on display for general aviation lightplanes /

Harris, Randall L.
Hewes, Donald E.
Langley Research Center.

January 1973

Prepared at Langley Research Center.Cover title.Includes bibliographical references (p. 27).Mode of ...

A rendezvous and station-keeping simulator with fly-around capability and virtual-image viewing /

Kahlbaum, William M.
Stumpf, John J.
Bardusch, Richard E.
United States. National Aeronautics and Space Administration.
Langley Research Center.

Prepared at Langley Research Center."April 1969"--Cover.Includes bibliographical references (p. 20)....

Air-helium simulation of the aerodynamic force coefficients of cones at hypersonic speeds /

Ladson, Charles L.
Blackstock, Thomas A.
United States. National Aeronautics and Space Administration.

Cover title."October 1962."Aerodynamics, missiles and space vehicles; Fluid mechanics; Simulators an...

Description of a 2-foot hypersonic facility at the Langley Research Center /

Stokes, George M.
Langley Research Center.

Prepared at Langley Research Center."September 1961."Cover title.Includes bibliographical references...

Effect of air contamination in a helium tunnel /

Henderson, Arthur, 1922-
Swalley, Frank E. (Frank Edwin), 1936-
Langley Research Center.

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

Ideal-gas tables for helium flow in the Mach number range from 40 to 100 /

Mueller, James N.
Langley Research Center.

Prepared at Langley Research Center."May 1962."Cover title.Includes bibliographical references (p. 6...

Transition fixing for hypersonic flow /

Sterrett, James R.
Langley Research Center.

Prepared at Langley Research Center."October 1967"--Cover.Includes bibliographical references (p. 12...

A simulation investigation of the loads experienced by a piloted launch vehicle /

Sleeper, Robert K.
Langley Research Center.

Prepared at Langley Research Center."March 1966"--Cover.Includes bibliographical references (p. 33)....

A study of equilibrium real-gas effects in hypersonic air nozzles, including charts of thermodynamic properties for equilibrium air /

Erickson, Wayne D. (Wayne Douglas), 1932-
Creekmore, Helen S.
Langley Research Center.

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

Aerodynamic testing technique for twin-fuselage models at hypersonic speeds /

Ashby, George C.
Langley Research Center.

January 1975

Prepared at Langley Research Center.Cover title.Includes bibliographical references (p. 6).Mode of a...

Structural concepts for hydrogen-fueled hypersonic airplanes /

Jackson, L. Robert.
Wichorek, Gregory R.
Davis, John G.
United States. National Aeronautics and Space Administration.
Langley Research Center.

"February 1966"--Cover.Includes bibliographical references.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 (...

Operating characteristics of the Langley Mach 10 high Reynolds number helium tunnel /

Watson, Ralph D.
Fischer, Michael C.
Morris, Dana J.
Langley Research Center.

January 1974

Prepared at Langley Research Center.Cover title.Includes bibliographical references (p. 10).Mode of ...

Fixed-base simulation study of a pilot's ability to control a winged-satellite vehicle during high-drag variable-lift entries /

Eggleston, John M. (John Marshall)
Cheatham, Donald C.
Baron, Sheldon.
Langley Research Center.

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

Loads induced on a flat plate at a Mach number of 4.5 with a sonic or supersonic jet exhausting normal to the surface /

Letko, William.
Langley Research Center.

Prepared at Langley Research Center."July 1963."Cover title.Includes bibliographical references (p. ...

An exploratory simulation study of a head-on display for general aviation lightplanes /

Harris, Randall L.
Hewes, Donald E.
Langley Research Center.

January 1973

Prepared at Langley Research Center.Cover title.Includes bibliographical references (p. 27).Mode of ...

A rendezvous and station-keeping simulator with fly-around capability and virtual-image viewing /

Kahlbaum, William M.
Stumpf, John J.
Bardusch, Richard E.
United States. National Aeronautics and Space Administration.
Langley Research Center.

Prepared at Langley Research Center."April 1969"--Cover.Includes bibliographical references (p. 20)....

Some aspects of air-helium simulation and hypersonic approximations /

Abstract

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Some aspects of air-helium simulation and hypersonic approximations /

Abstract

Extracted data

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