Inlet sensitivity study for a supersonic transport /

Measurement of performance, inlet flow characteristics, and radiated noise for a turbojet engine having choked inlet flow /

Cawthorn, Jimmy M.
Hayes, Clyde.
Morris, Garland J.
United States. National Aeronautics and Space Administration.
Langley Research Center.

January 1967

Performed at Langley Research Center."May 1967."Includes bibliographical references (p. 16).Mode of ...

Concentration measurements of an injected gas in a supersonic stream /

Torrence, Marvin G.
Langley Research Center.

Prepared at Langley Research Center."April 1967"--Cover.Includes bibliographical references (p. 11)....

Experimental investigation of the partial- admission performance characteristics of a single-stage Mach 2 supersonic turbine /

Moffitt, Thomas P.
Klag, Frederick W.
Langley Research Center.

January 1959

"September 1959."Cover title.Includes bibliographical references (p. 8).Mode of access: Internet

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

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

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

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

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

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

Flow and wall-temperature sensitivity in parallel passages for large inlet to exit density ratios in subsonic flow /

Reshotko, Meyer.
Lewis Research Center.
United States. National Aeronautics and Space Administration.

January 1968

Cover title."July 1968."Includes bibliographical references (p. 28).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

Low-speed performance of an axisymmetric, mixed-compression, supersonic inlet with auxiliary inlets /

Trefny, Charles J.
Wasserbauer, Joseph W.
Lewis Research Center.

January 1986

Prepared at Lewis Research Center."February 1986"--Cover.Includes bibliographical references (p. 10)...

Aerodynamic and acoustic performance of high Mach number inlets /

Lumsdaine, Edward.
United States. National Aeronautics and Space Administration.

January 1977

Issued Aug. 1977.Includes bibliographical references (p. 12-15).Mode of access: Internet

Mechanical characteristics of stability-bleed valves for a supersonic inlet /

Neiner, George H.
Cole, Gary L., joint author.
Dustin, Miles O., joint author.
United States. National Aeronautics and Space Administration.

January 1977

Issued Dec. 1977.Includes bibliographical references (p. 17-18).Mode of access: Internet

Transonic pressure distributions over protuberances and adjacent areas in proximity to the nose of a launch vehicle /

Blackwell, James A.
Langley Research Center.
United States. National Aeronautics and Space Administration.

January 1966

Cover title."March 1966."Includes bibliographical references (p. 7).Mode of access: Internet

Measurement of performance, inlet flow characteristics, and radiated noise for a turbojet engine having choked inlet flow /

Cawthorn, Jimmy M.
Hayes, Clyde.
Morris, Garland J.
United States. National Aeronautics and Space Administration.
Langley Research Center.

January 1967

Performed at Langley Research Center."May 1967."Includes bibliographical references (p. 16).Mode of ...

Concentration measurements of an injected gas in a supersonic stream /

Torrence, Marvin G.
Langley Research Center.

Prepared at Langley Research Center."April 1967"--Cover.Includes bibliographical references (p. 11)....

Experimental investigation of the partial- admission performance characteristics of a single-stage Mach 2 supersonic turbine /

Moffitt, Thomas P.
Klag, Frederick W.
Langley Research Center.

January 1959

"September 1959."Cover title.Includes bibliographical references (p. 8).Mode of access: Internet

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

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

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

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

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

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

Flow and wall-temperature sensitivity in parallel passages for large inlet to exit density ratios in subsonic flow /

Reshotko, Meyer.
Lewis Research Center.
United States. National Aeronautics and Space Administration.

January 1968

Cover title."July 1968."Includes bibliographical references (p. 28).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

Low-speed performance of an axisymmetric, mixed-compression, supersonic inlet with auxiliary inlets /

Trefny, Charles J.
Wasserbauer, Joseph W.
Lewis Research Center.

January 1986

Prepared at Lewis Research Center."February 1986"--Cover.Includes bibliographical references (p. 10)...

Aerodynamic and acoustic performance of high Mach number inlets /

Lumsdaine, Edward.
United States. National Aeronautics and Space Administration.

January 1977

Issued Aug. 1977.Includes bibliographical references (p. 12-15).Mode of access: Internet

Mechanical characteristics of stability-bleed valves for a supersonic inlet /

Neiner, George H.
Cole, Gary L., joint author.
Dustin, Miles O., joint author.
United States. National Aeronautics and Space Administration.

January 1977

Issued Dec. 1977.Includes bibliographical references (p. 17-18).Mode of access: Internet

Transonic pressure distributions over protuberances and adjacent areas in proximity to the nose of a launch vehicle /

Blackwell, James A.
Langley Research Center.
United States. National Aeronautics and Space Administration.

January 1966

Cover title."March 1966."Includes bibliographical references (p. 7).Mode of access: Internet

Measurement of performance, inlet flow characteristics, and radiated noise for a turbojet engine having choked inlet flow /

Cawthorn, Jimmy M.
Hayes, Clyde.
Morris, Garland J.
United States. National Aeronautics and Space Administration.
Langley Research Center.

January 1967

Performed at Langley Research Center."May 1967."Includes bibliographical references (p. 16).Mode of ...

Concentration measurements of an injected gas in a supersonic stream /

Torrence, Marvin G.
Langley Research Center.

Prepared at Langley Research Center."April 1967"--Cover.Includes bibliographical references (p. 11)....

Experimental investigation of the partial- admission performance characteristics of a single-stage Mach 2 supersonic turbine /

Moffitt, Thomas P.
Klag, Frederick W.
Langley Research Center.

January 1959

"September 1959."Cover title.Includes bibliographical references (p. 8).Mode of access: Internet

Inlet sensitivity study for a supersonic transport /

Abstract

Extracted data

Inlet sensitivity study for a supersonic transport /

Abstract

Extracted data

Related items

Related items