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

Application of sonic-boom minimization concepts in supersonic transport design /

Carlson, Harry W.
Mack, Robert J.
Barger, Raymond L.
Langley Research Center.

January 1973

Prepared at Langley Research Center.Cover title.Bibliography: p. 42-44.Mode of access: Internet

Numerical methods for the design and analysis of wings at supersonic speeds /

Carlson, Harry W.
Miller, David S.
Langley Research Center.

January 1974

Prepared at Langley Research Center.Cover title.Includes bibliographical references (p. 29-30).Mode ...

Stability and control characteristics of an air-breathing missile configuration having a forward located inlet /

Sawyer, Wallace C.
Hayes, Clyde.
Langley Research Center.

January 1976

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

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 ...

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...

Design of a bleed system for a Mach 3.5 inlet /

Syberg, J.
Hickcox, T. E.
Ames Research Center.
Boeing Company.

January 1973

"Prepared by the Boeing Company ... for Ames Research Center."Cover title.Bibliography: p. 32.Mode o...

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 ...

Operating characteristics of the Langley Mach 7 Scramjet Test Facility /

Guy, Robert W.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.
Langley Research Center.

January 1981

"March 1981"--Cover."Langley Research Center."Includes bibliographical references.Mode of access: In...

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 ...

Performance of a hydrogen burner to simulate air entering scramjet combustors /

Russin, William Roger.
Langley Research Center.

January 1974

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

Validation of scramjet exhaust simulation technique at Mach 6 /

Hopkins, H. B.
Leng, J.
Konopka, W.
Langley Research Center.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Office.

January 1979

"Prepared for Langley Research Center under contract NAS1-14152."Includes bibliographical references...

Operating characteristics of the Langley Mach 10 high Reynolds number helium tunnel /

Watson, Ralph D.
Fischer, Michael C.
Morris, Dana J.
Langley Research Center.

January 1974

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

Description of a 2-foot hypersonic facility at the Langley Research Center /

Stokes, George M.
Langley Research Center.

Prepared at Langley Research Center."September 1961."Cover title.Includes bibliographical references...

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

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...

Application of sonic-boom minimization concepts in supersonic transport design /

Carlson, Harry W.
Mack, Robert J.
Barger, Raymond L.
Langley Research Center.

January 1973

Prepared at Langley Research Center.Cover title.Bibliography: p. 42-44.Mode of access: Internet

Numerical methods for the design and analysis of wings at supersonic speeds /

Carlson, Harry W.
Miller, David S.
Langley Research Center.

January 1974

Prepared at Langley Research Center.Cover title.Includes bibliographical references (p. 29-30).Mode ...

Stability and control characteristics of an air-breathing missile configuration having a forward located inlet /

Sawyer, Wallace C.
Hayes, Clyde.
Langley Research Center.

January 1976

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

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 ...

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...

Design of a bleed system for a Mach 3.5 inlet /

Syberg, J.
Hickcox, T. E.
Ames Research Center.
Boeing Company.

January 1973

"Prepared by the Boeing Company ... for Ames Research Center."Cover title.Bibliography: p. 32.Mode o...

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 ...

Operating characteristics of the Langley Mach 7 Scramjet Test Facility /

Guy, Robert W.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.
Langley Research Center.

January 1981

"March 1981"--Cover."Langley Research Center."Includes bibliographical references.Mode of access: In...

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 ...

Performance of a hydrogen burner to simulate air entering scramjet combustors /

Russin, William Roger.
Langley Research Center.

January 1974

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

Validation of scramjet exhaust simulation technique at Mach 6 /

Hopkins, H. B.
Leng, J.
Konopka, W.
Langley Research Center.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Office.

January 1979

"Prepared for Langley Research Center under contract NAS1-14152."Includes bibliographical references...

Operating characteristics of the Langley Mach 10 high Reynolds number helium tunnel /

Watson, Ralph D.
Fischer, Michael C.
Morris, Dana J.
Langley Research Center.

January 1974

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

Description of a 2-foot hypersonic facility at the Langley Research Center /

Stokes, George M.
Langley Research Center.

Prepared at Langley Research Center."September 1961."Cover title.Includes bibliographical references...

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

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...

Application of sonic-boom minimization concepts in supersonic transport design /

Carlson, Harry W.
Mack, Robert J.
Barger, Raymond L.
Langley Research Center.

January 1973

Prepared at Langley Research Center.Cover title.Bibliography: p. 42-44.Mode of access: Internet

Numerical methods for the design and analysis of wings at supersonic speeds /

Carlson, Harry W.
Miller, David S.
Langley Research Center.

January 1974

Prepared at Langley Research Center.Cover title.Includes bibliographical references (p. 29-30).Mode ...

Stability and control characteristics of an air-breathing missile configuration having a forward located inlet /

Sawyer, Wallace C.
Hayes, Clyde.
Langley Research Center.

January 1976

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

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

Abstract

Extracted data

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

Abstract

Extracted data

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