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

Wind-tunnel investigation of an upper surface blown jet-flap powered-lift configuration /

Phelps, Arthur E.
Smith, Charles Christian, 1921-
Langley Research Center.

January 1973

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

A study for development of aerothermodynamic test model materials and fabrication technique /

Dean, W. G.
Connor, L. E.
Langley Research Center.
Lockheed Missiles and Space Company.

January 1972

"Prepared by Lockheed Missiles & Space Company ... for Langley Research Center."Cover title.Bibliogr...

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...

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 ...

Hypersonic aerodynamics and entry-maneuver--aerothermodynamic interactions for two lifting entry vehicles /

Arrington, James P.
Woods, William C.
Langley Research Center.

January 1972

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

Analysis of transonic flow about lifting wing-body configurations /

Barnwell, Richard W.
Langley Research Center.

January 1975

Prepared at Langley Research Center.Cover title.Includes bibliographical references (p. 69-71).Mode ...

Design and performance at a local Mach number of 6 of an inlet for an integrated scramjet concept /

Trexler, Carl A. (Carl Arthur), 1942-
Souders, Sue W.
Langley Research Center.

January 1975

Prepared at Langley Research Center.Cover title.Includes bibliographical references (p. 50).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

Wind-tunnel investigation of a twin-engine straight-wing upper-surface blown jet-flap configuration /

Phelps, Arthur E.
Langley Research Center.

January 1975

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

Thermal dynamic modeling study /

Ojalvo, I. U.
Langley Research Center.
Grumman Aerospace Corporation.

January 1972

"Prepared by Grumman Aerospace Corporation ... for Langley Research Center."Cover title.Bibliography...

Design and performance of the University of Michigan 6.6-inch hypersonic wind tunnel /

Amick, James L.
Langley Research Center.
University of Michigan.

January 1975

"Prepared by the University of Michigan ... for Langley Research Center."Cover title.Includes biblio...

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...

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

Conceptual study of a turbojet/ramjet inlet /

Weidner, John P. (John Patrick), 1938-
Langley Research Center.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.

January 1979

Subject category 07."September 1979"--Cover."Langley Research Center."Mode of access: Internet

Wind-tunnel investigation of an upper surface blown jet-flap powered-lift configuration /

Phelps, Arthur E.
Smith, Charles Christian, 1921-
Langley Research Center.

January 1973

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

A study for development of aerothermodynamic test model materials and fabrication technique /

Dean, W. G.
Connor, L. E.
Langley Research Center.
Lockheed Missiles and Space Company.

January 1972

"Prepared by Lockheed Missiles & Space Company ... for Langley Research Center."Cover title.Bibliogr...

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...

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 ...

Hypersonic aerodynamics and entry-maneuver--aerothermodynamic interactions for two lifting entry vehicles /

Arrington, James P.
Woods, William C.
Langley Research Center.

January 1972

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

Analysis of transonic flow about lifting wing-body configurations /

Barnwell, Richard W.
Langley Research Center.

January 1975

Prepared at Langley Research Center.Cover title.Includes bibliographical references (p. 69-71).Mode ...

Design and performance at a local Mach number of 6 of an inlet for an integrated scramjet concept /

Trexler, Carl A. (Carl Arthur), 1942-
Souders, Sue W.
Langley Research Center.

January 1975

Prepared at Langley Research Center.Cover title.Includes bibliographical references (p. 50).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

Wind-tunnel investigation of a twin-engine straight-wing upper-surface blown jet-flap configuration /

Phelps, Arthur E.
Langley Research Center.

January 1975

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

Thermal dynamic modeling study /

Ojalvo, I. U.
Langley Research Center.
Grumman Aerospace Corporation.

January 1972

"Prepared by Grumman Aerospace Corporation ... for Langley Research Center."Cover title.Bibliography...

Design and performance of the University of Michigan 6.6-inch hypersonic wind tunnel /

Amick, James L.
Langley Research Center.
University of Michigan.

January 1975

"Prepared by the University of Michigan ... for Langley Research Center."Cover title.Includes biblio...

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...

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

Conceptual study of a turbojet/ramjet inlet /

Weidner, John P. (John Patrick), 1938-
Langley Research Center.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.

January 1979

Subject category 07."September 1979"--Cover."Langley Research Center."Mode of access: Internet

Wind-tunnel investigation of an upper surface blown jet-flap powered-lift configuration /

Phelps, Arthur E.
Smith, Charles Christian, 1921-
Langley Research Center.

January 1973

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

A study for development of aerothermodynamic test model materials and fabrication technique /

Dean, W. G.
Connor, L. E.
Langley Research Center.
Lockheed Missiles and Space Company.

January 1972

"Prepared by Lockheed Missiles & Space Company ... for Langley Research Center."Cover title.Bibliogr...

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...

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

Abstract

Extracted data

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

Abstract

Extracted data

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