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

A method for designing low-drag nose-inlet-body combinations for operation at moderate supersonic speeds /

Howell, Robert R.
Langley Aeronautical Laboratory.
United States. National Adviosry Committee for Aeronautics. NACA research memorandum.

January 1954

"November 24, 1954."Includes bibliographical references (p. 13).Mode of access: Internet

Performance of experimental channeled-wall annular turbojet combustor at conditions simulating high-altitude supersonic flight.

Zettle, Eugene V.
Friedman, Robert, 1929-
Lewis Flight Propulsion Laboratory.
United States. National Adviosry Committee for Aeronautics. NACA research memorandum.
United States. National Advisory Committee for Aeronautics.

January 1955

"March 15, 1955."Includes bibliographical references (p. 7).Mode of access: Internet

An evaluation of two cooling-air ejectors in flight at transonic speeds /

Rolls, L. Stewart
Havill, C. Dewey, joint author.
United States. National Advisory Committee for Aeronautics. NACA research memorandum.
Ames Research Center.

On front cover: "March 15, 1954."Includes bibliographical references.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

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

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 investigation of a disk-shaped reentry configuration at transonic and low supersonic speeds /

Lazzeroni, Frank A.
United States. National Aeronautics and Space Administration.

"May 1962."Cover title.Includes bibliographical references (p. 7).Mode of access: Internet

Investigation at transonic speeds of aerodynamic characteristics of an unswept semielliptical air inlet in the root of a 45©� sweptback wing /

Bingham, Gene J.
Langley Aeronautical Laboratory.
United States. National Adviosry Committee for Aeronautics. NACA research memorandum.

January 1955

"September 28, 1955."Includes bibliographical references (p. 16).Mode of access: Internet

Simulated altitude performance of two annular combustors with continuous axial openings for admission of primary air /

Zettle, Eugene V.
Mark, Herman, joint author.
United States. National Advisory Committee for Aeronautics. NACA research memorandum.
Lewis Flight Propulsion Laboratory.

On front cover: "August 3, 1950."Includes bibliographical references: p. 12.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

Wind-tunnel studies at subsonic and transonic speeds of a multiple-mission variable-wing- sweep airplane configuration /

Alford, William J.
Handerson, William P.
Luoma, Arvo A.
Langley Research Center.

January 1959

"November 1959."Cover title.Includes bibliographical references (p. 13).Mode of access: Internet

Experimental investigation of flow through three highly loaded inlet guide vanes having different spanwise circulation gradients /

Beatty, Loren A.
Emery, James C.
Savage, Melvyn.
Langley Aeronautical Laboratory.
United States. National Adviosry Committee for Aeronautics. NACA research memorandum.
United States. National Advisory Committee for Aeronautics.

January 1952

"July 28, 1952."Cover title.Includes bibliographical references (p. 12).Mode of access: Internet

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

Transonic wind-tunnel investigation of an unswept wing in combination with a systematic series of four bodies /

Estabrooks, Bruce B.
Langley Aeronautical Laboratory.
United States. National Adviosry Committee for Aeronautics. NACA research memorandum.

January 1953

"Janauary 6, 1953."Includes bibliographical references (p. 11).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

A method for designing low-drag nose-inlet-body combinations for operation at moderate supersonic speeds /

Howell, Robert R.
Langley Aeronautical Laboratory.
United States. National Adviosry Committee for Aeronautics. NACA research memorandum.

January 1954

"November 24, 1954."Includes bibliographical references (p. 13).Mode of access: Internet

Performance of experimental channeled-wall annular turbojet combustor at conditions simulating high-altitude supersonic flight.

Zettle, Eugene V.
Friedman, Robert, 1929-
Lewis Flight Propulsion Laboratory.
United States. National Adviosry Committee for Aeronautics. NACA research memorandum.
United States. National Advisory Committee for Aeronautics.

January 1955

"March 15, 1955."Includes bibliographical references (p. 7).Mode of access: Internet

An evaluation of two cooling-air ejectors in flight at transonic speeds /

Rolls, L. Stewart
Havill, C. Dewey, joint author.
United States. National Advisory Committee for Aeronautics. NACA research memorandum.
Ames Research Center.

On front cover: "March 15, 1954."Includes bibliographical references.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

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

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 investigation of a disk-shaped reentry configuration at transonic and low supersonic speeds /

Lazzeroni, Frank A.
United States. National Aeronautics and Space Administration.

"May 1962."Cover title.Includes bibliographical references (p. 7).Mode of access: Internet

Investigation at transonic speeds of aerodynamic characteristics of an unswept semielliptical air inlet in the root of a 45©� sweptback wing /

Bingham, Gene J.
Langley Aeronautical Laboratory.
United States. National Adviosry Committee for Aeronautics. NACA research memorandum.

January 1955

"September 28, 1955."Includes bibliographical references (p. 16).Mode of access: Internet

Simulated altitude performance of two annular combustors with continuous axial openings for admission of primary air /

Zettle, Eugene V.
Mark, Herman, joint author.
United States. National Advisory Committee for Aeronautics. NACA research memorandum.
Lewis Flight Propulsion Laboratory.

On front cover: "August 3, 1950."Includes bibliographical references: p. 12.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

Wind-tunnel studies at subsonic and transonic speeds of a multiple-mission variable-wing- sweep airplane configuration /

Alford, William J.
Handerson, William P.
Luoma, Arvo A.
Langley Research Center.

January 1959

"November 1959."Cover title.Includes bibliographical references (p. 13).Mode of access: Internet

Experimental investigation of flow through three highly loaded inlet guide vanes having different spanwise circulation gradients /

Beatty, Loren A.
Emery, James C.
Savage, Melvyn.
Langley Aeronautical Laboratory.
United States. National Adviosry Committee for Aeronautics. NACA research memorandum.
United States. National Advisory Committee for Aeronautics.

January 1952

"July 28, 1952."Cover title.Includes bibliographical references (p. 12).Mode of access: Internet

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

Transonic wind-tunnel investigation of an unswept wing in combination with a systematic series of four bodies /

Estabrooks, Bruce B.
Langley Aeronautical Laboratory.
United States. National Adviosry Committee for Aeronautics. NACA research memorandum.

January 1953

"Janauary 6, 1953."Includes bibliographical references (p. 11).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

A method for designing low-drag nose-inlet-body combinations for operation at moderate supersonic speeds /

Howell, Robert R.
Langley Aeronautical Laboratory.
United States. National Adviosry Committee for Aeronautics. NACA research memorandum.

January 1954

"November 24, 1954."Includes bibliographical references (p. 13).Mode of access: Internet

Performance of experimental channeled-wall annular turbojet combustor at conditions simulating high-altitude supersonic flight.

Zettle, Eugene V.
Friedman, Robert, 1929-
Lewis Flight Propulsion Laboratory.
United States. National Adviosry Committee for Aeronautics. NACA research memorandum.
United States. National Advisory Committee for Aeronautics.

January 1955

"March 15, 1955."Includes bibliographical references (p. 7).Mode of access: Internet

An evaluation of two cooling-air ejectors in flight at transonic speeds /

Rolls, L. Stewart
Havill, C. Dewey, joint author.
United States. National Advisory Committee for Aeronautics. NACA research memorandum.
Ames Research Center.

On front cover: "March 15, 1954."Includes bibliographical references.Mode of access: Internet

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

Abstract

Extracted data

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

Abstract

Extracted data

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