Analysis of a bypass air control system for a supersonic mixed-compression inlet /

Experimental pressure distributions on a blunt lifting-entry body at Mach 3.71 /

Morris, W. Douglas.
Couch, Lana M.
Langley Research Center.
United States. National Aeronautics and Space Administration.

January 1968

Cover title."April 1968."Includes bibliographical references (p. 12).Mode of access: Internet

Investigation of a retrorocket exhausting from the nose of a blunt body into a supersonic free stream /

Charczenko, Nickolai.
Hennessey, Katherine W.
United States. National Aeronautics and Space Administration.

Cover title."September 1961."Aerodynamics, missiles and space vehicles; Atmospheric entry.Includes b...

An analytical investigation of the aerodynamic and performance characteristics of an unpowered rotor entry vehicle /

Levin, Alan D.
Smith, Ronald C.
Ames Research Center.
United States. National Aeronautics and Space Administration.

January 1968

Cover title."April 1968."Includes bibliographical references (p. 18).Mode of access: Internet

Bypass-duct design for use with supersonic inlets /

Wood, Charles C.
Henry, John R.
Langley Aeronautical Laboratory.
United States. National Adviosry Committee for Aeronautics. NACA research memorandum.

January 1956

"March 16, 1956".Includes bibliographical references (p. 6).Mode of access: Internet

Considerations of turbine cooling systems for Mach 3 flight /

Stepka, Francis S.
Lewis Research Center.
United States. National Aeronautics and Space Administration.

January 1968

Cover title."April 1968."Includes bibliographical references (p. 32).Mode of access: Internet

Inlet sensitivity study for a supersonic transport /

Koenig, Robert W.
Lewis Research Center.
United States. National Aeronautics and Space Administration.

"March 1967."Includes bibliographical references (p. 52).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

Dynamics of a supersonic inlet with adjustable bypass in combination with a J34 turbojet engine /

Wilcox, Fred.
Whalen, Paul.
Lewis Flight Propulsion Laboratory.
United States. National Adviosry Committee for Aeronautics. NACA research memorandum.
United States. National Advisory Committee for Aeronautics.

"Declassified February 10, 1959.""March 23, 1956."Cover title.Includes bibliographical references (p...

Development of a three-dimensional supersonic inlet flow analysis /

Buggeln, R. C.
Lewis Research Center.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Office.

January 1980

"January 1980"--Cover.Includes bibliographical references.Mode of access: Internet

Statistical analysis of landing-contact conditions for the XB-70 airplane /

Wilson, Ronald J.
Larson, Richard R.
Flight Research Center (U.S.)
United States. National Aeronautics and Space Administration.

January 1967

Cover title."June 1967."Includes bibliographical references (p. 11).Mode of access: Internet

Investigation of pitch maneuver speed margins for a supersonic transport configuration with a variable-sweep wing /

Sawyer, Richard H.
Silsby, Norman S.
McLaughlin, Milton D.
United States. National Aeronautics and Space Administration.
Langley Research Center.

January 1967

"October 1967."Includes bibliographical references (p. 15).Mode of access: Internet

The performance of conical supersonic scoop inlets on circular fuselages /

Hasel, Lowell E.
Langley Aeronautical Laboratory.
United States. National Adviosry Committee for Aeronautics. NACA research memorandum.

January 1953

"November 17, 1953."Includes bibliographical references (p. 7).Mode of access: Internet

Investigation over moving ground plane of a transport airplane model using blowing over flaps for boundary-layer control /

Vogler, Raymond D.
Langley Research Center.
United States. National Aeronautics and Space Administration.

January 1967

Cover title."August 1967."Includes bibliographical references (p. 10).Mode of access: Internet

Transition fixing for hypersonic flow /

Sterrett, James R.
Langley Research Center.

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

Stability analysis and minimum thrust vector control requirements of booster vehicles during atmospheric flight /

Borsody, Janos.
Teren, Fred.
Lewis Research Center.
United States. National Aeronautics and Space Administration.

January 1968

Cover title."May 1968."Includes bibliographical references (p. 42).Mode of access: Internet

Experimental pressure distributions on a blunt lifting-entry body at Mach 3.71 /

Morris, W. Douglas.
Couch, Lana M.
Langley Research Center.
United States. National Aeronautics and Space Administration.

January 1968

Cover title."April 1968."Includes bibliographical references (p. 12).Mode of access: Internet

Investigation of a retrorocket exhausting from the nose of a blunt body into a supersonic free stream /

Charczenko, Nickolai.
Hennessey, Katherine W.
United States. National Aeronautics and Space Administration.

Cover title."September 1961."Aerodynamics, missiles and space vehicles; Atmospheric entry.Includes b...

An analytical investigation of the aerodynamic and performance characteristics of an unpowered rotor entry vehicle /

Levin, Alan D.
Smith, Ronald C.
Ames Research Center.
United States. National Aeronautics and Space Administration.

January 1968

Cover title."April 1968."Includes bibliographical references (p. 18).Mode of access: Internet

Bypass-duct design for use with supersonic inlets /

Wood, Charles C.
Henry, John R.
Langley Aeronautical Laboratory.
United States. National Adviosry Committee for Aeronautics. NACA research memorandum.

January 1956

"March 16, 1956".Includes bibliographical references (p. 6).Mode of access: Internet

Considerations of turbine cooling systems for Mach 3 flight /

Stepka, Francis S.
Lewis Research Center.
United States. National Aeronautics and Space Administration.

January 1968

Cover title."April 1968."Includes bibliographical references (p. 32).Mode of access: Internet

Inlet sensitivity study for a supersonic transport /

Koenig, Robert W.
Lewis Research Center.
United States. National Aeronautics and Space Administration.

"March 1967."Includes bibliographical references (p. 52).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

Dynamics of a supersonic inlet with adjustable bypass in combination with a J34 turbojet engine /

Wilcox, Fred.
Whalen, Paul.
Lewis Flight Propulsion Laboratory.
United States. National Adviosry Committee for Aeronautics. NACA research memorandum.
United States. National Advisory Committee for Aeronautics.

"Declassified February 10, 1959.""March 23, 1956."Cover title.Includes bibliographical references (p...

Development of a three-dimensional supersonic inlet flow analysis /

Buggeln, R. C.
Lewis Research Center.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Office.

January 1980

"January 1980"--Cover.Includes bibliographical references.Mode of access: Internet

Statistical analysis of landing-contact conditions for the XB-70 airplane /

Wilson, Ronald J.
Larson, Richard R.
Flight Research Center (U.S.)
United States. National Aeronautics and Space Administration.

January 1967

Cover title."June 1967."Includes bibliographical references (p. 11).Mode of access: Internet

Investigation of pitch maneuver speed margins for a supersonic transport configuration with a variable-sweep wing /

Sawyer, Richard H.
Silsby, Norman S.
McLaughlin, Milton D.
United States. National Aeronautics and Space Administration.
Langley Research Center.

January 1967

"October 1967."Includes bibliographical references (p. 15).Mode of access: Internet

The performance of conical supersonic scoop inlets on circular fuselages /

Hasel, Lowell E.
Langley Aeronautical Laboratory.
United States. National Adviosry Committee for Aeronautics. NACA research memorandum.

January 1953

"November 17, 1953."Includes bibliographical references (p. 7).Mode of access: Internet

Investigation over moving ground plane of a transport airplane model using blowing over flaps for boundary-layer control /

Vogler, Raymond D.
Langley Research Center.
United States. National Aeronautics and Space Administration.

January 1967

Cover title."August 1967."Includes bibliographical references (p. 10).Mode of access: Internet

Transition fixing for hypersonic flow /

Sterrett, James R.
Langley Research Center.

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

Stability analysis and minimum thrust vector control requirements of booster vehicles during atmospheric flight /

Borsody, Janos.
Teren, Fred.
Lewis Research Center.
United States. National Aeronautics and Space Administration.

January 1968

Cover title."May 1968."Includes bibliographical references (p. 42).Mode of access: Internet

Experimental pressure distributions on a blunt lifting-entry body at Mach 3.71 /

Morris, W. Douglas.
Couch, Lana M.
Langley Research Center.
United States. National Aeronautics and Space Administration.

January 1968

Cover title."April 1968."Includes bibliographical references (p. 12).Mode of access: Internet

Investigation of a retrorocket exhausting from the nose of a blunt body into a supersonic free stream /

Charczenko, Nickolai.
Hennessey, Katherine W.
United States. National Aeronautics and Space Administration.

Cover title."September 1961."Aerodynamics, missiles and space vehicles; Atmospheric entry.Includes b...

An analytical investigation of the aerodynamic and performance characteristics of an unpowered rotor entry vehicle /

Levin, Alan D.
Smith, Ronald C.
Ames Research Center.
United States. National Aeronautics and Space Administration.

January 1968

Cover title."April 1968."Includes bibliographical references (p. 18).Mode of access: Internet

Analysis of a bypass air control system for a supersonic mixed-compression inlet /

Abstract

Extracted data

Analysis of a bypass air control system for a supersonic mixed-compression inlet /

Abstract

Extracted data

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