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

Theoretical and experimental internal flow characteristics of a 13.97-centimeter-diameter inlet at STOL takeoff and approach conditions /

Albers, James A.
Lewis Research Center.

January 1973

Prepared at Lewis Research Center.Cover title.Bibliography: p. 12.Mode of access: Internet

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 ...

A simulator study for the development and evaluation of operating procedures on a supersonic cruise research transport to minimize airport-community noise /

Grantham, William D.
Deal, Perry L.
Smith, Paul M., 1931-
Langley Research Center.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.

January 1980

Nov. 1980."Langley Research Center."Includes bibliographical references.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 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...

Cruise performance of an isolated 1.15 pressure ratio turbofan propulsion system simulator at Mach numbers from 0.6 to 0.85 /

Steffen, Fred W.
Lewis Research Center.

January 1974

Prepared at Lewis Research Center.Cover title.Includes bibliographical references (p. 22).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...

Subsonic annular wing theory with application to flow about nacelles /

Mann, Michael J.
Langley Research Center.

January 1974

Prepared at Langley Research Center.Cover title.Includes bibliographical references (p. 90-91).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

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

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 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

Experimental and analytical study of an inlet forebody for an airframe-integrated scramjet concept /

Andrews, Earl H.
Pinckney, S. Z. (Shimer Zane), 1934-
Agnone, Anthony M.
Langley Research Center.

January 1975

Prepared at Langley Research Center.Cover title.Includes bibliographical references (p. 23-25).Mode ...

Subsonic wind-tunnel investigation of a twin-engine attack airplane model having nonmetric powered nacelles /

Lockwood, Vernard E.
Matarazzo, Aniello.
Langley Research Center.

January 1974

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

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 ...

Theoretical and experimental internal flow characteristics of a 13.97-centimeter-diameter inlet at STOL takeoff and approach conditions /

Albers, James A.
Lewis Research Center.

January 1973

Prepared at Lewis Research Center.Cover title.Bibliography: p. 12.Mode of access: Internet

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 ...

A simulator study for the development and evaluation of operating procedures on a supersonic cruise research transport to minimize airport-community noise /

Grantham, William D.
Deal, Perry L.
Smith, Paul M., 1931-
Langley Research Center.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.

January 1980

Nov. 1980."Langley Research Center."Includes bibliographical references.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 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...

Cruise performance of an isolated 1.15 pressure ratio turbofan propulsion system simulator at Mach numbers from 0.6 to 0.85 /

Steffen, Fred W.
Lewis Research Center.

January 1974

Prepared at Lewis Research Center.Cover title.Includes bibliographical references (p. 22).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...

Subsonic annular wing theory with application to flow about nacelles /

Mann, Michael J.
Langley Research Center.

January 1974

Prepared at Langley Research Center.Cover title.Includes bibliographical references (p. 90-91).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

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

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 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

Experimental and analytical study of an inlet forebody for an airframe-integrated scramjet concept /

Andrews, Earl H.
Pinckney, S. Z. (Shimer Zane), 1934-
Agnone, Anthony M.
Langley Research Center.

January 1975

Prepared at Langley Research Center.Cover title.Includes bibliographical references (p. 23-25).Mode ...

Subsonic wind-tunnel investigation of a twin-engine attack airplane model having nonmetric powered nacelles /

Lockwood, Vernard E.
Matarazzo, Aniello.
Langley Research Center.

January 1974

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

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 ...

Theoretical and experimental internal flow characteristics of a 13.97-centimeter-diameter inlet at STOL takeoff and approach conditions /

Albers, James A.
Lewis Research Center.

January 1973

Prepared at Lewis Research Center.Cover title.Bibliography: p. 12.Mode of access: Internet

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 ...

A simulator study for the development and evaluation of operating procedures on a supersonic cruise research transport to minimize airport-community noise /

Grantham, William D.
Deal, Perry L.
Smith, Paul M., 1931-
Langley Research Center.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.

January 1980

Nov. 1980."Langley Research Center."Includes bibliographical references.Mode of access: Internet

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

Abstract

Extracted data

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

Abstract

Extracted data

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