The performance of conical supersonic scoop inlets on circular fuselages /

Investigation of the performance of a turbojet engine with variable-position compressor inlet guide vanes /

Budinger, Ray E.
Kaufman, Harold R.
Lewis Flight Propulsion Laboratory.
United States. National Adviosry Committee for Aeronautics. NACA research memorandum.

January 1955

"October 4, 1955."Includes bibliographical references (p. 20).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

Load distributions associated with controls at supersonic speeds /

Czarnecki, K. R.
Lord, Douglas R.
Langley Aeronautical Laboratory.
United States. National Adviosry Committee for Aeronautics. NACA research memorandum.

January 1953

"May 29, 1953."Includes bibliographical references (p. 13).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

Some considerations concerning inlets and ducted bodies at Mach numbers from 0.8 to 2.0 /

Sears, Richard I.
Langley Aeronautical Laboratory.
United States. National Adviosry Committee for Aeronautics. NACA research memorandum.

January 1953

"November 24, 1953."Includes bibliographical references (p. 10-11).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

Effect of yaw and angle of attack on pressure recovery and mass-flow characteristics of a rectangular supersonic scoop inlet at a Mach number of 2.71 /

Comenzo, Raymond J.
Mackley, Ernest A.
Langley Aeronautical Laboratory.
United States. National Adviosry Committee for Aeronautics. NACA research memorandum.
United States. National Advisory Committee for Aeronautics.

January 1954

"September 10, 1954."Includes bibliographical references (p. 7).Mode of access: Internet

Investigation of an underslung half-cone inlet with compression surface mounted outboard from fuselage at mach numbers of 1.5, 1.8, and 2.0 /

Yeager, Richard A.
Gertsma, Laurence W.
Lewis Flight Propulsion Laboratory.
United States. National Adviosry Committee for Aeronautics. NACA research memorandum.

January 1958

"May 12, 1958."Includes bibliographical references (p. 7).Mode of access: Internet

Performance of external-compression bump inlet at Mach numbers of 1.5 to 2.0 /

Simon, Paul C.
Huff, Ronald G.
Brown, Dennis W.
Lewis Flight Propulsion Laboratory.
United States. National Adviosry Committee for Aeronautics. NACA research memorandum.

January 1957

"April 24, 1957."Includes bibliographical references (p. 9).Mode of access: Internet

An experimental study of five annular air inlet configurations at subsonic and transonic speeds /

Bryan, Carroll R.
Fleming, Frank F.
Milillo, Jospeh R.
Pendley, Robert E.
Langley Aeronautical Laboratory.
United States. National Adviosry Committee for Aeronautics. NACA research memorandum.

January 1953

"August 19, 1953."Includes bibliographical references (p. 22-23).Mode of access: Internet

Aerodynamic characteristics of a modified cone : conical-frustum entry configuration at Mach 6.0 /

Ashby, George C.
Staylor, W. Frank.
Langley Research Center.
United States. National Aeronautics and Space Administration.

January 1968

Cover title."June 1968."Includes bibliographical references (p. 8).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

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

Brown, Stuart C.
United States. National Aeronautics and Space Administration.

Cover title."June 1967."Includes bibliographical references.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...

Preliminary results of supersonic-jet tests of simplified wing structures /

Heldenfels, Richard R.
Rosecrans, Richard.
Langley Aeronautical Laboratory.
United States. National Adviosry Committee for Aeronautics. NACA research memorandum.

January 1953

"July 8, 1953."Includes bibliographical references (p. 15).Mode of access: Internet

Investigation of the performance of a turbojet engine with variable-position compressor inlet guide vanes /

Budinger, Ray E.
Kaufman, Harold R.
Lewis Flight Propulsion Laboratory.
United States. National Adviosry Committee for Aeronautics. NACA research memorandum.

January 1955

"October 4, 1955."Includes bibliographical references (p. 20).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

Load distributions associated with controls at supersonic speeds /

Czarnecki, K. R.
Lord, Douglas R.
Langley Aeronautical Laboratory.
United States. National Adviosry Committee for Aeronautics. NACA research memorandum.

January 1953

"May 29, 1953."Includes bibliographical references (p. 13).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

Some considerations concerning inlets and ducted bodies at Mach numbers from 0.8 to 2.0 /

Sears, Richard I.
Langley Aeronautical Laboratory.
United States. National Adviosry Committee for Aeronautics. NACA research memorandum.

January 1953

"November 24, 1953."Includes bibliographical references (p. 10-11).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

Effect of yaw and angle of attack on pressure recovery and mass-flow characteristics of a rectangular supersonic scoop inlet at a Mach number of 2.71 /

Comenzo, Raymond J.
Mackley, Ernest A.
Langley Aeronautical Laboratory.
United States. National Adviosry Committee for Aeronautics. NACA research memorandum.
United States. National Advisory Committee for Aeronautics.

January 1954

"September 10, 1954."Includes bibliographical references (p. 7).Mode of access: Internet

Investigation of an underslung half-cone inlet with compression surface mounted outboard from fuselage at mach numbers of 1.5, 1.8, and 2.0 /

Yeager, Richard A.
Gertsma, Laurence W.
Lewis Flight Propulsion Laboratory.
United States. National Adviosry Committee for Aeronautics. NACA research memorandum.

January 1958

"May 12, 1958."Includes bibliographical references (p. 7).Mode of access: Internet

Performance of external-compression bump inlet at Mach numbers of 1.5 to 2.0 /

Simon, Paul C.
Huff, Ronald G.
Brown, Dennis W.
Lewis Flight Propulsion Laboratory.
United States. National Adviosry Committee for Aeronautics. NACA research memorandum.

January 1957

"April 24, 1957."Includes bibliographical references (p. 9).Mode of access: Internet

An experimental study of five annular air inlet configurations at subsonic and transonic speeds /

Bryan, Carroll R.
Fleming, Frank F.
Milillo, Jospeh R.
Pendley, Robert E.
Langley Aeronautical Laboratory.
United States. National Adviosry Committee for Aeronautics. NACA research memorandum.

January 1953

"August 19, 1953."Includes bibliographical references (p. 22-23).Mode of access: Internet

Aerodynamic characteristics of a modified cone : conical-frustum entry configuration at Mach 6.0 /

Ashby, George C.
Staylor, W. Frank.
Langley Research Center.
United States. National Aeronautics and Space Administration.

January 1968

Cover title."June 1968."Includes bibliographical references (p. 8).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

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

Brown, Stuart C.
United States. National Aeronautics and Space Administration.

Cover title."June 1967."Includes bibliographical references.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...

Preliminary results of supersonic-jet tests of simplified wing structures /

Heldenfels, Richard R.
Rosecrans, Richard.
Langley Aeronautical Laboratory.
United States. National Adviosry Committee for Aeronautics. NACA research memorandum.

January 1953

"July 8, 1953."Includes bibliographical references (p. 15).Mode of access: Internet

Investigation of the performance of a turbojet engine with variable-position compressor inlet guide vanes /

Budinger, Ray E.
Kaufman, Harold R.
Lewis Flight Propulsion Laboratory.
United States. National Adviosry Committee for Aeronautics. NACA research memorandum.

January 1955

"October 4, 1955."Includes bibliographical references (p. 20).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

Load distributions associated with controls at supersonic speeds /

Czarnecki, K. R.
Lord, Douglas R.
Langley Aeronautical Laboratory.
United States. National Adviosry Committee for Aeronautics. NACA research memorandum.

January 1953

"May 29, 1953."Includes bibliographical references (p. 13).Mode of access: Internet

The performance of conical supersonic scoop inlets on circular fuselages /

Abstract

Extracted data

The performance of conical supersonic scoop inlets on circular fuselages /

Abstract

Extracted data

Related items

Related items