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

Pressure distributions for a rectangular supersonic inlet at subsonic speeds /

Fuller, Dennis E.
Langley Research Center.

January 1976

Research prepared at Langley Research Center.Cover title.Bibliography: p. 9.Mode of access: Internet

Experimental evaluation of a Mach 3.5 axisymmetric inlet /

Syberg, J.
Koncsek, J. L.
Ames Research Center.
Boeing Commercial Airplane Company.

"Prepared by Boeing Commercial Airplane Company ... for Ames Research Center.""July 1975."Cover titl...

Experimental cavity pressure distributions at supersonic speeds /

Stallings, Robert L.
Wilcox, Floyd J. (Floyd Jay)
Langley Research Center.

January 1987

Prepared at Langley Research Center."June 1987"--Cover.Includes bibliographical references (p. 9).Mo...

Transonic off-design drag and performance of three mixed-compression axisymmetric inlets /

Woollett, Richard R.
Choby, David A.
Meleason, Edward T.
Lewis Research Center.

January 1975

Prepared at Lewis Research Center.Cover title.Includes bibliographical references (p. 17).Mode of ac...

Design of a very-low-bleed Mach 2.5 mixed-compression inlet with 45 percent internal contraction /

Wasserbauer, Joseph F.
Neumann, Harvey E.
Shaw, Robert J. (Robert Joseph), 1946-
Lewis Research Center.

January 1975

Prepared at Lewis Research Center.Cover title.Includes bibliographical references (p. 25).Mode of ac...

Transonic performance of a Mach 2.65 auxiliary flow axisymmetric inlet /

Santman, Don M.
United States. National Aeronautics and Space Administration.
Ames Research Center.
Ellco Engineering, Inc.

January 1976

Issued Oct. 1976.Cover title.Includes bibliographical references (p. 16).Mode of access: Internet

Performance of a Mach Number 3.0 design axisymmetric double-cone external-compression inlet in the mach number range 1.97 to 0.79 /

Davis, Owen H.
Mitchell, Glenn A.
Lewis Research Center.

January 1960

"Lewis Research Center, Cleveland, Ohio.""N 63-16136.""April 1960"--Cover.Includes bibliographical r...

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

Performance of inlet stage of transonic compressor /

Urasek, Donald C.
Lewis, George W., Jr.
Steinke, Ronald J.
Lewis Research Center.

January 1976

Prepared at Lewis Research Center.Cover title.Includes bibliographical references (p. 17).Mode of ac...

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

Performance summary and analysis of a Mach 3.0 design axisymmetric all-external-compression double-cone inlet Mach number range 3.0 to 0.8 /

Allen, John L.
Mitchell, Glenn A.
Davis, Owen H.
Lewis Research Center.

January 1960

"Lewis Research Center, Cleveland, Ohio.""N 63-16135.""April 1960"--Cover.Includes bibliographical r...

Performance of centerbody vortex generators in an axisymmetric mixed-compression inlet at Mach numbers from 2.0 to 3.0 /

Mitchell, Glen A.
Davis, Ronald W.
Lewis Research Center.
United States. National Aeronautics and Space Administration.

January 1968

Cover title."July 1968."Includes bibliographical references (p. 12).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

Performance of vortex generators in a Mach 2.5 low-bleed full-scale 45-percent-internal-contraction axisymmetric inlet /

Neumann, Harvey E.
Shaw, Robert J. (Robert Joseph), 1946-
Wasserbauer, Joseph F.
Lewis Research Center.

January 1975

Prepared at Lewis Research Center.Cover title.Includes bibliographical references (p. 17).Mode of ac...

Performance of a turbojet engine in combination with an external-internal-compression inlet to mach 2.88 /

Bowditch, David N.
Tabata, William K.
Anderson, Bernhard H.
United States. National Aeronautics and Space Administration.

"July 1960."Cover title.Includes bibliographical references (p. 10-11).Mode of access: Internet

Pressure distributions for a rectangular supersonic inlet at subsonic speeds /

Fuller, Dennis E.
Langley Research Center.

January 1976

Research prepared at Langley Research Center.Cover title.Bibliography: p. 9.Mode of access: Internet

Experimental evaluation of a Mach 3.5 axisymmetric inlet /

Syberg, J.
Koncsek, J. L.
Ames Research Center.
Boeing Commercial Airplane Company.

"Prepared by Boeing Commercial Airplane Company ... for Ames Research Center.""July 1975."Cover titl...

Experimental cavity pressure distributions at supersonic speeds /

Stallings, Robert L.
Wilcox, Floyd J. (Floyd Jay)
Langley Research Center.

January 1987

Prepared at Langley Research Center."June 1987"--Cover.Includes bibliographical references (p. 9).Mo...

Transonic off-design drag and performance of three mixed-compression axisymmetric inlets /

Woollett, Richard R.
Choby, David A.
Meleason, Edward T.
Lewis Research Center.

January 1975

Prepared at Lewis Research Center.Cover title.Includes bibliographical references (p. 17).Mode of ac...

Design of a very-low-bleed Mach 2.5 mixed-compression inlet with 45 percent internal contraction /

Wasserbauer, Joseph F.
Neumann, Harvey E.
Shaw, Robert J. (Robert Joseph), 1946-
Lewis Research Center.

January 1975

Prepared at Lewis Research Center.Cover title.Includes bibliographical references (p. 25).Mode of ac...

Transonic performance of a Mach 2.65 auxiliary flow axisymmetric inlet /

Santman, Don M.
United States. National Aeronautics and Space Administration.
Ames Research Center.
Ellco Engineering, Inc.

January 1976

Issued Oct. 1976.Cover title.Includes bibliographical references (p. 16).Mode of access: Internet

Performance of a Mach Number 3.0 design axisymmetric double-cone external-compression inlet in the mach number range 1.97 to 0.79 /

Davis, Owen H.
Mitchell, Glenn A.
Lewis Research Center.

January 1960

"Lewis Research Center, Cleveland, Ohio.""N 63-16136.""April 1960"--Cover.Includes bibliographical r...

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

Performance of inlet stage of transonic compressor /

Urasek, Donald C.
Lewis, George W., Jr.
Steinke, Ronald J.
Lewis Research Center.

January 1976

Prepared at Lewis Research Center.Cover title.Includes bibliographical references (p. 17).Mode of ac...

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

Performance summary and analysis of a Mach 3.0 design axisymmetric all-external-compression double-cone inlet Mach number range 3.0 to 0.8 /

Allen, John L.
Mitchell, Glenn A.
Davis, Owen H.
Lewis Research Center.

January 1960

"Lewis Research Center, Cleveland, Ohio.""N 63-16135.""April 1960"--Cover.Includes bibliographical r...

Performance of centerbody vortex generators in an axisymmetric mixed-compression inlet at Mach numbers from 2.0 to 3.0 /

Mitchell, Glen A.
Davis, Ronald W.
Lewis Research Center.
United States. National Aeronautics and Space Administration.

January 1968

Cover title."July 1968."Includes bibliographical references (p. 12).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

Performance of vortex generators in a Mach 2.5 low-bleed full-scale 45-percent-internal-contraction axisymmetric inlet /

Neumann, Harvey E.
Shaw, Robert J. (Robert Joseph), 1946-
Wasserbauer, Joseph F.
Lewis Research Center.

January 1975

Prepared at Lewis Research Center.Cover title.Includes bibliographical references (p. 17).Mode of ac...

Performance of a turbojet engine in combination with an external-internal-compression inlet to mach 2.88 /

Bowditch, David N.
Tabata, William K.
Anderson, Bernhard H.
United States. National Aeronautics and Space Administration.

"July 1960."Cover title.Includes bibliographical references (p. 10-11).Mode of access: Internet

Pressure distributions for a rectangular supersonic inlet at subsonic speeds /

Fuller, Dennis E.
Langley Research Center.

January 1976

Research prepared at Langley Research Center.Cover title.Bibliography: p. 9.Mode of access: Internet

Experimental evaluation of a Mach 3.5 axisymmetric inlet /

Syberg, J.
Koncsek, J. L.
Ames Research Center.
Boeing Commercial Airplane Company.

"Prepared by Boeing Commercial Airplane Company ... for Ames Research Center.""July 1975."Cover titl...

Experimental cavity pressure distributions at supersonic speeds /

Stallings, Robert L.
Wilcox, Floyd J. (Floyd Jay)
Langley Research Center.

January 1987

Prepared at Langley Research Center."June 1987"--Cover.Includes bibliographical references (p. 9).Mo...

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

Abstract

Extracted data

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

Abstract

Extracted data

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