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

A study of methods which predict supersonic flow fields from body geometry, distance, and Mach number /

Mack, Robert J.
Langley Research Center.

January 1973

Prepared at Langley Research Center.Cover title.Includes bibliographical references (p. 13-14).Mode ...

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 /

Hawkins, J. E.
Turner, R. L. (Ralph Lilley), Sir, 1888-1983, joint author.
Kirkland, F. P., joint author.
Ames Research Center.
General Dynamics Corporation. Convair Aerospace Division.
United States. National Aeronautics and Space Administration.

January 1976

Cover title.Includes bibliographical references (p. 46).Mode of access: Internet

Evaluation of mean and turbulent velocity measurements in subsonic accelerated boundary layers /

Sandborn, V. A.
Seegmiller, H. L., joint author.
Ames Research Center.

January 1976

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

Control of shock wave - boundary layer interactions by bleed in supersonic mixed compression inlets /

Fukuda, Michael K.
Reshotko, Eli.
Hingst, Warren R.
Lewis Research Center.
Case Western Reserve University.

January 1975

Cover title.Includes bibliographical references (p. 131-133).Mode of access: Internet

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...

Analytical and experimental performance of optimal controller designs for a supersonic inlet /

Zeller, John R.
Lewis Research Center.

January 1973

Prepared at Lewis Research Center.Cover title.Bibliography: p. 84-85.Mode of access: Internet

Analysis of a stability valve system for extending the dynamic range of a supersonic inlet /

Webb, John A.
Dustin, Miles O.
Lewis Research Center.

January 1975

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

Weak incident shock interactions with Mach 8 laminar boundary layers /

Kaufman, Louis G.
Johnson, Charles B.
Langley Research Center.

January 1974

Prepared at Langley Research Center.Cover title.Includes bibliographical references (p. 21-23).Mode ...

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

Performance and boundary-layer evaluation of a sonic inlet /

Schmidt, James F.
Ruggeri, Robert S., joint author.
Lewis Research Center.

January 1976

Cover title.Includes bibliographical references (p. 25).Mode of access: Internet

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...

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

A short static-pressure probe design for supersonic flow /

Pinckney, S. Z. (Shimer Zane), 1934-
Langley Research Center.

January 1975

Prepared at Langley Research Center.Cover title.Includes bibliographical references (p. 10-11).Mode ...

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 ...

Assessment of an analytical procedure for predicting supersonic ejector nozzle performance /

Anderson, Bernhard H.
Lewis Research Center.

January 1974

Prepared at Lewis Research Center.Cover title.Includes bibliographical references (p. 13-14).Mode of...

A study of methods which predict supersonic flow fields from body geometry, distance, and Mach number /

Mack, Robert J.
Langley Research Center.

January 1973

Prepared at Langley Research Center.Cover title.Includes bibliographical references (p. 13-14).Mode ...

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 /

Hawkins, J. E.
Turner, R. L. (Ralph Lilley), Sir, 1888-1983, joint author.
Kirkland, F. P., joint author.
Ames Research Center.
General Dynamics Corporation. Convair Aerospace Division.
United States. National Aeronautics and Space Administration.

January 1976

Cover title.Includes bibliographical references (p. 46).Mode of access: Internet

Evaluation of mean and turbulent velocity measurements in subsonic accelerated boundary layers /

Sandborn, V. A.
Seegmiller, H. L., joint author.
Ames Research Center.

January 1976

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

Control of shock wave - boundary layer interactions by bleed in supersonic mixed compression inlets /

Fukuda, Michael K.
Reshotko, Eli.
Hingst, Warren R.
Lewis Research Center.
Case Western Reserve University.

January 1975

Cover title.Includes bibliographical references (p. 131-133).Mode of access: Internet

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...

Analytical and experimental performance of optimal controller designs for a supersonic inlet /

Zeller, John R.
Lewis Research Center.

January 1973

Prepared at Lewis Research Center.Cover title.Bibliography: p. 84-85.Mode of access: Internet

Analysis of a stability valve system for extending the dynamic range of a supersonic inlet /

Webb, John A.
Dustin, Miles O.
Lewis Research Center.

January 1975

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

Weak incident shock interactions with Mach 8 laminar boundary layers /

Kaufman, Louis G.
Johnson, Charles B.
Langley Research Center.

January 1974

Prepared at Langley Research Center.Cover title.Includes bibliographical references (p. 21-23).Mode ...

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

Performance and boundary-layer evaluation of a sonic inlet /

Schmidt, James F.
Ruggeri, Robert S., joint author.
Lewis Research Center.

January 1976

Cover title.Includes bibliographical references (p. 25).Mode of access: Internet

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...

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

A short static-pressure probe design for supersonic flow /

Pinckney, S. Z. (Shimer Zane), 1934-
Langley Research Center.

January 1975

Prepared at Langley Research Center.Cover title.Includes bibliographical references (p. 10-11).Mode ...

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 ...

Assessment of an analytical procedure for predicting supersonic ejector nozzle performance /

Anderson, Bernhard H.
Lewis Research Center.

January 1974

Prepared at Lewis Research Center.Cover title.Includes bibliographical references (p. 13-14).Mode of...

A study of methods which predict supersonic flow fields from body geometry, distance, and Mach number /

Mack, Robert J.
Langley Research Center.

January 1973

Prepared at Langley Research Center.Cover title.Includes bibliographical references (p. 13-14).Mode ...

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 /

Hawkins, J. E.
Turner, R. L. (Ralph Lilley), Sir, 1888-1983, joint author.
Kirkland, F. P., joint author.
Ames Research Center.
General Dynamics Corporation. Convair Aerospace Division.
United States. National Aeronautics and Space Administration.

January 1976

Cover title.Includes bibliographical references (p. 46).Mode of access: Internet

Evaluation of mean and turbulent velocity measurements in subsonic accelerated boundary layers /

Sandborn, V. A.
Seegmiller, H. L., joint author.
Ames Research Center.

January 1976

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

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

Abstract

Extracted data

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

Abstract

Extracted data

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