Inlet spillage drag tests and numerical flow-field analysis at subsonic and transonic speeds of a 1/8-scale, two-dimensional, external-compression, variable-geometry supersonic inlet configuration /

Effect of subsonic inlet lip geometry on predicted surface and flow Mach number distributions /

Albers, James A.
Miller, Brent A.
Lewis Research Center.

January 1973

Prepared at Lewis Research Center.Cover title.Includes bibliographical references (p. 16).Mode of ac...

Low-speed investigation of the aerodynamic characteristics of a variable-sweep supersonic transport configuration having a blended wing and body /

Sleeman, William C.
Robins, A. Warner.
Langley Research Center.

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

An Inlet analysis for the NASA hypersonic research engine aerothermodynamic integration model /

Andrews, Earl H.
Langley Research Center.

January 1974

Prepared at Langley Research Center.Cover title.Includes bibliographical references (p. 20).Mode of ...

Analysis of the dynamic response of a supersonic inlet to flow-field perturbations upstream of the normal shock /

Cole, Gary L.
Willoh, Ross G.
Lewis Research Center.

January 1975

Prepared at Lewis Research Center.Cover title.Includes bibliographical references (p. 26-27).Mode of...

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

Calculation of two-dimensional inlet flow fields in a supersonic free stream : program documentation and test cases /

Biringen, Sedat.
McMillan, Oden J.
Langley Research Center.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Office.

January 1980

"March 1980"--Cover.Includes bibliographical references.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

Inlet spillage drag tests and numerical flow-field analysis at subsonic and transonic speeds of a 1/8-scale, two-dimensional, external-compression, variable-geometry, supersonic inlet configuration

Kirkland, F. P.
Hawkins, J. E.
Turner, R. L.

April 1976

Accurate spillage drag and pressure data are presented for a realistic supersonic inlet configuratio...

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...

Evaluation of some control-volume techniques for analysis of shock-boundary-layer interactions in supersonic inlets /

Hingst, Warren R.
Lewis Research Center.

January 1975

Prepared at Lewis Research Center.Cover title.Includes bibliographical references (p. 9).Mode of acc...

Experimental investigation of a large-scale, two-dimensional, mixed-compression inlet system : internal performance and drag at transonic conditions, M[infinity]=0.6 to 1.28 / by Norman D. Wong and Warren E. Anderson.

Wong, Norman D.
Anderson, Warren E.
Ames Research Center.

January 1973

Prepared at Ames Research Center.Cover title.Includes bibliographical references (p. 12).Mode of acc...

Low-speed wind-tunnel investigation of the aerodynamic and acoustic performance of a translating-grid choked-flow inlet /

Abbott, John M.
Golladay, Richard L.
Miller, Brent A.
Lewis Research Center.

January 1974

Prepared at Lewis Research Center.Cover title.Includes bibliographical references (p. 15-16).Mode of...

Use of potential flow theory to evaluate subsonic inlet data from a simulator-powered nacelle at cruise conditions /

Bober, Lawrence J.
Lewis Research Center.

January 1974

Prepared at Lewis Research Center.Cover title.Includes bibliographical references (p. 12-14).Mode of...

Analysis of experimental results of the inlet for the NASA hypersonic research engine aerothermodynamic integration model /

Andrews, Earl H.
Mackley, Ernest A., joint author.
United States. National Aeronautics and Space Administration.
Langley Research Center.

January 1976

Cover title.Includes bibliographical references (p. 26-27).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)...

Effect of subsonic inlet lip geometry on predicted surface and flow Mach number distributions /

Albers, James A.
Miller, Brent A.
Lewis Research Center.

January 1973

Prepared at Lewis Research Center.Cover title.Includes bibliographical references (p. 16).Mode of ac...

Low-speed investigation of the aerodynamic characteristics of a variable-sweep supersonic transport configuration having a blended wing and body /

Sleeman, William C.
Robins, A. Warner.
Langley Research Center.

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

An Inlet analysis for the NASA hypersonic research engine aerothermodynamic integration model /

Andrews, Earl H.
Langley Research Center.

January 1974

Prepared at Langley Research Center.Cover title.Includes bibliographical references (p. 20).Mode of ...

Analysis of the dynamic response of a supersonic inlet to flow-field perturbations upstream of the normal shock /

Cole, Gary L.
Willoh, Ross G.
Lewis Research Center.

January 1975

Prepared at Lewis Research Center.Cover title.Includes bibliographical references (p. 26-27).Mode of...

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

Calculation of two-dimensional inlet flow fields in a supersonic free stream : program documentation and test cases /

Biringen, Sedat.
McMillan, Oden J.
Langley Research Center.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Office.

January 1980

"March 1980"--Cover.Includes bibliographical references.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

Inlet spillage drag tests and numerical flow-field analysis at subsonic and transonic speeds of a 1/8-scale, two-dimensional, external-compression, variable-geometry, supersonic inlet configuration

Kirkland, F. P.
Hawkins, J. E.
Turner, R. L.

April 1976

Accurate spillage drag and pressure data are presented for a realistic supersonic inlet configuratio...

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...

Evaluation of some control-volume techniques for analysis of shock-boundary-layer interactions in supersonic inlets /

Hingst, Warren R.
Lewis Research Center.

January 1975

Prepared at Lewis Research Center.Cover title.Includes bibliographical references (p. 9).Mode of acc...

Experimental investigation of a large-scale, two-dimensional, mixed-compression inlet system : internal performance and drag at transonic conditions, M[infinity]=0.6 to 1.28 / by Norman D. Wong and Warren E. Anderson.

Wong, Norman D.
Anderson, Warren E.
Ames Research Center.

January 1973

Prepared at Ames Research Center.Cover title.Includes bibliographical references (p. 12).Mode of acc...

Low-speed wind-tunnel investigation of the aerodynamic and acoustic performance of a translating-grid choked-flow inlet /

Abbott, John M.
Golladay, Richard L.
Miller, Brent A.
Lewis Research Center.

January 1974

Prepared at Lewis Research Center.Cover title.Includes bibliographical references (p. 15-16).Mode of...

Use of potential flow theory to evaluate subsonic inlet data from a simulator-powered nacelle at cruise conditions /

Bober, Lawrence J.
Lewis Research Center.

January 1974

Prepared at Lewis Research Center.Cover title.Includes bibliographical references (p. 12-14).Mode of...

Analysis of experimental results of the inlet for the NASA hypersonic research engine aerothermodynamic integration model /

Andrews, Earl H.
Mackley, Ernest A., joint author.
United States. National Aeronautics and Space Administration.
Langley Research Center.

January 1976

Cover title.Includes bibliographical references (p. 26-27).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)...

Effect of subsonic inlet lip geometry on predicted surface and flow Mach number distributions /

Albers, James A.
Miller, Brent A.
Lewis Research Center.

January 1973

Prepared at Lewis Research Center.Cover title.Includes bibliographical references (p. 16).Mode of ac...

Low-speed investigation of the aerodynamic characteristics of a variable-sweep supersonic transport configuration having a blended wing and body /

Sleeman, William C.
Robins, A. Warner.
Langley Research Center.

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

An Inlet analysis for the NASA hypersonic research engine aerothermodynamic integration model /

Andrews, Earl H.
Langley Research Center.

January 1974

Prepared at Langley Research Center.Cover title.Includes bibliographical references (p. 20).Mode of ...

Inlet spillage drag tests and numerical flow-field analysis at subsonic and transonic speeds of a 1/8-scale, two-dimensional, external-compression, variable-geometry supersonic inlet configuration /

Abstract

Extracted data

Inlet spillage drag tests and numerical flow-field analysis at subsonic and transonic speeds of a 1/8-scale, two-dimensional, external-compression, variable-geometry supersonic inlet configuration /

Abstract

Extracted data

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