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

Design operation and testing capabilities of the Langley 11-inch ceramic-heated tunnel

Trout, Otto F.
United States. National Aeronautics and Space Administration.

Cover title."February 1963."Includes bibliographical references.Mode of access: Internet

Some aspects of air-helium simulation and hypersonic approximations /

Love, Eugene S.
Bertram, Mitchel H.
Henderson, Arthur, 1922-
Langley Research Center.

Prepared at Langley Research Center."October 1959."Cover title.Includes bibliographical references (...

Description and calibration of the Langley hypersonic CF₄ tunnel : a facility for simulating low [gamma] flow as occurs for a real gas /

Midden, Raymond E.
Miller, Charles G. (Charles George), 1940-
Langley Research Center.

January 1985

Prepared at Langley Research Center."March 1985"--Cover.Includes bibliographical references (p. 16)....

Design and performance of the University of Michigan 6.6-inch hypersonic wind tunnel /

Amick, James L.
Langley Research Center.
University of Michigan.

January 1975

"Prepared by the University of Michigan ... for Langley Research Center."Cover title.Includes biblio...

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. ...

The Cryogenic wind-tunnel concept for high Reynolds number testing /

Kilgore, Robert A.
Langley Research Center.

January 1974

Prepared at Langley Research Center.Cover title.Includes bibliographical references (p. 53-55).Mode ...

Operating characteristics of the Langley Mach 7 Scramjet Test Facility /

Guy, Robert W.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.
Langley Research Center.

January 1981

"March 1981"--Cover."Langley Research Center."Includes bibliographical references.Mode of access: In...

Description and calibration of the Langley 6- by 19-inch transonic tunnel /

Ladson, Charles L.
Langley Research Center.

January 1973

Prepared at Langley Research Center.Cover title.Bibliography: p. 16-17.Mode of access: Internet

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...

Wind-tunnel investigation of an upper surface blown jet-flap powered-lift configuration /

Phelps, Arthur E.
Smith, Charles Christian, 1921-
Langley Research Center.

January 1973

Prepared at Langley Research Center.Cover title.Includes bibliographical references (p. 11).Mode of ...

Effect of a variable-geometry diffuser on the operating characteristics of a helium tunnel designed for a mach number in excess of 20 /

Johnston, Patrick J.
Witcofski, Robert D.
Langley Research Center.

January 1960

"NASA TN D-237.""Langley Research Center, Langley Field, Va.""February 1960."Cover title.Includes bi...

Design and performance at a local Mach number of 6 of an inlet for an integrated scramjet concept /

Trexler, Carl A. (Carl Arthur), 1942-
Souders, Sue W.
Langley Research Center.

January 1975

Prepared at Langley Research Center.Cover title.Includes bibliographical references (p. 50).Mode of ...

High-speed flow past wings /

Nørstrud, Helge, 1934-
Langley Research Center.
Lockheed-Georgia Company.

January 1973

"Prepared by Lockheed-Georgia Company ... for Langley Research Center."Cover title.Bibliography: p. ...

Calibration of the Langley 16-foot transonic tunnel with test section air removal /

Corson, Blake W.
Igoe, William B.
Runckel, Jack F.
Langley Research Center.

January 1974

Prepared at Langley Research Center.Cover title.Includes bibliographical references (p. 38-39).Mode ...

Wind-tunnel investigation of a twin-engine straight-wing upper-surface blown jet-flap configuration /

Phelps, Arthur E.
Langley Research Center.

January 1975

Prepared at Langley Research Center.Cover title.Includes bibliographical references (p. 15).Mode of ...

Design operation and testing capabilities of the Langley 11-inch ceramic-heated tunnel

Trout, Otto F.
United States. National Aeronautics and Space Administration.

Cover title."February 1963."Includes bibliographical references.Mode of access: Internet

Some aspects of air-helium simulation and hypersonic approximations /

Love, Eugene S.
Bertram, Mitchel H.
Henderson, Arthur, 1922-
Langley Research Center.

Prepared at Langley Research Center."October 1959."Cover title.Includes bibliographical references (...

Description and calibration of the Langley hypersonic CF₄ tunnel : a facility for simulating low [gamma] flow as occurs for a real gas /

Midden, Raymond E.
Miller, Charles G. (Charles George), 1940-
Langley Research Center.

January 1985

Prepared at Langley Research Center."March 1985"--Cover.Includes bibliographical references (p. 16)....

Design and performance of the University of Michigan 6.6-inch hypersonic wind tunnel /

Amick, James L.
Langley Research Center.
University of Michigan.

January 1975

"Prepared by the University of Michigan ... for Langley Research Center."Cover title.Includes biblio...

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. ...

The Cryogenic wind-tunnel concept for high Reynolds number testing /

Kilgore, Robert A.
Langley Research Center.

January 1974

Prepared at Langley Research Center.Cover title.Includes bibliographical references (p. 53-55).Mode ...

Operating characteristics of the Langley Mach 7 Scramjet Test Facility /

Guy, Robert W.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.
Langley Research Center.

January 1981

"March 1981"--Cover."Langley Research Center."Includes bibliographical references.Mode of access: In...

Description and calibration of the Langley 6- by 19-inch transonic tunnel /

Ladson, Charles L.
Langley Research Center.

January 1973

Prepared at Langley Research Center.Cover title.Bibliography: p. 16-17.Mode of access: Internet

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...

Wind-tunnel investigation of an upper surface blown jet-flap powered-lift configuration /

Phelps, Arthur E.
Smith, Charles Christian, 1921-
Langley Research Center.

January 1973

Prepared at Langley Research Center.Cover title.Includes bibliographical references (p. 11).Mode of ...

Effect of a variable-geometry diffuser on the operating characteristics of a helium tunnel designed for a mach number in excess of 20 /

Johnston, Patrick J.
Witcofski, Robert D.
Langley Research Center.

January 1960

"NASA TN D-237.""Langley Research Center, Langley Field, Va.""February 1960."Cover title.Includes bi...

Design and performance at a local Mach number of 6 of an inlet for an integrated scramjet concept /

Trexler, Carl A. (Carl Arthur), 1942-
Souders, Sue W.
Langley Research Center.

January 1975

Prepared at Langley Research Center.Cover title.Includes bibliographical references (p. 50).Mode of ...

High-speed flow past wings /

Nørstrud, Helge, 1934-
Langley Research Center.
Lockheed-Georgia Company.

January 1973

"Prepared by Lockheed-Georgia Company ... for Langley Research Center."Cover title.Bibliography: p. ...

Calibration of the Langley 16-foot transonic tunnel with test section air removal /

Corson, Blake W.
Igoe, William B.
Runckel, Jack F.
Langley Research Center.

January 1974

Prepared at Langley Research Center.Cover title.Includes bibliographical references (p. 38-39).Mode ...

Wind-tunnel investigation of a twin-engine straight-wing upper-surface blown jet-flap configuration /

Phelps, Arthur E.
Langley Research Center.

January 1975

Prepared at Langley Research Center.Cover title.Includes bibliographical references (p. 15).Mode of ...

Design operation and testing capabilities of the Langley 11-inch ceramic-heated tunnel

Trout, Otto F.
United States. National Aeronautics and Space Administration.

Cover title."February 1963."Includes bibliographical references.Mode of access: Internet

Some aspects of air-helium simulation and hypersonic approximations /

Love, Eugene S.
Bertram, Mitchel H.
Henderson, Arthur, 1922-
Langley Research Center.

Prepared at Langley Research Center."October 1959."Cover title.Includes bibliographical references (...

Description and calibration of the Langley hypersonic CF₄ tunnel : a facility for simulating low [gamma] flow as occurs for a real gas /

Midden, Raymond E.
Miller, Charles G. (Charles George), 1940-
Langley Research Center.

January 1985

Prepared at Langley Research Center."March 1985"--Cover.Includes bibliographical references (p. 16)....

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

Abstract

Extracted data

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

Abstract

Extracted data

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