Effects of vibrational nonequilibrium on the inviscid design of an axisymmetric nozzle for hypersonic flow /

Effects of nozzle interfairing modifications on longitudinal aerodynamic characteristics of a twin-jet, variable-wing-sweep fighter model /

Reubush, David E.
Mercer, Charles E.
Langley Research Center.

January 1975

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

Investigation of Axisymmetric and nonaxisymmetric nozzels installed on a 0.10-scale F-18 protype airplane model /

Capone, Francis J.
Berrier, Bobby L.
Langley Research Center.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Office.

January 1980

"Subject Category 02.""Langley Research Center.""June 1980"--Cover.Includes bibliographical referenc...

Second-order small-disturbance solutions for hypersonic flow over power-law bodies /

Townsend, James C. (James Courtland), 1938-
Langley Research Center.

January 1975

Prepared at Langley Research Center.Cover title.Includes bibliographical references (p. 57-58).Mode ...

A study of equilibrium real-gas effects in hypersonic air nozzles, including charts of thermodynamic properties for equilibrium air /

Erickson, Wayne D. (Wayne Douglas), 1932-
Creekmore, Helen S.
Langley Research Center.

Prepared at Langley Research Center."April 1960."Cover title.Includes bibliographical references (p....

Chemical nonequilibrium effects on the inviscid flow in the windward plane of symmetry of two simplified shuttle configurations /

Lordi, John A.
Johnson, Charles B.
Vidal, Robert J.
Langley Research Center.

January 1973

Prepared at Langley Research Center.Cover title.Bibliography: p. 18-19.Mode of access: Internet

Static performance of an axisymmetric nozzle with post-exit vanes for multiaxis thrust vectoring /

Berrier, Bobby L.
Langley Research Center.

January 1988

Prepared at Langley Research Center."May 1988"--Cover.Includes bibliographical references (p. 11).Mo...

Experimental and analytical investigation of axisymmetric supersonic cruise nozzle geometry at Mach numbers form 0.60 to 1.30 /

Carson, George T.
Lee, Edwin E.
Langley Research Center.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.

January 1981

"December 1981"--Cover."Langley Research Center."Includes bibiliographical references.Mode of access...

Viscous-inviscid calculations of jet entrainment effects on the subsonic flow over nozzle afterbodies /

Wilmoth, Richard G.
Langley Research Center.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Office.

January 1980

Subject category 02."April 1980"--Cover."Langley Research Center."Includes bibliographical reference...

Effect of several geometric parameters on the static internal performance of three nonaxisymmetric nozzle concepts /

Berrier, Bobby L.
Re, Richard J.
Langley Research Center.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.

January 1979

Subject category 02.Includes statistical tables."July 1979"--Cover."Langley Research Center."Include...

Design of an axisymmetric, hypersonic nozzle, utilizing the method of characteristics

Bailey, Vincent Patrick, 1928-
Bailey, Vincent Patrick, 1928-

January 1962

This item was digitized from a paper original and/or a microfilm copy. If you need higher-resolution...

Static performance of nonaxisymmetric nozzles with yaw thrust-vectoring vanes /

Mason, Mary L.
Berrier, Bobby L.
Langley Research Center.

January 1988

Prepared at Langley Research Center."May 1988"--Cover.Includes bibliographical references (p. 10).Mo...

Effect of empennage arrangement on single-engine nozzle/afterbody static pressures at transonic speeds /

Henderson, William P.
Burley, James R.
Langley Research Center.

January 1987

Prepared at Langley Research Center."November 1987"--Cover.Includes bibliographical references (p. 7...

A preliminary assessment of the impact of 2-D exhaust-nozzle geometry on the cruise range of a hypersonic aircraft with top-mounted ramjet propulsion /

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

January 1980

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

A parametric study of effect of forebody shape on flow angularity at Mach 8 /

Johnson, Charles B.
Marcum, Don C.
Langley Research Center.

January 1974

Prepared at Langley Research Center.Cover title.Includes bibliographical references (p. 12-13).Mode ...

Hypersonic aerodynamic characteristics of a family of power-law, wing-body configuratioons /

Townsend, James C. (James Courtland), 1938-
Langley Research Center.

January 1973

Prepared at Langley Research Center.Cover title.Includes bibliographical references (p. 33-34).Mode ...

Effects of nozzle interfairing modifications on longitudinal aerodynamic characteristics of a twin-jet, variable-wing-sweep fighter model /

Reubush, David E.
Mercer, Charles E.
Langley Research Center.

January 1975

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

Investigation of Axisymmetric and nonaxisymmetric nozzels installed on a 0.10-scale F-18 protype airplane model /

Capone, Francis J.
Berrier, Bobby L.
Langley Research Center.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Office.

January 1980

"Subject Category 02.""Langley Research Center.""June 1980"--Cover.Includes bibliographical referenc...

Second-order small-disturbance solutions for hypersonic flow over power-law bodies /

Townsend, James C. (James Courtland), 1938-
Langley Research Center.

January 1975

Prepared at Langley Research Center.Cover title.Includes bibliographical references (p. 57-58).Mode ...

A study of equilibrium real-gas effects in hypersonic air nozzles, including charts of thermodynamic properties for equilibrium air /

Erickson, Wayne D. (Wayne Douglas), 1932-
Creekmore, Helen S.
Langley Research Center.

Prepared at Langley Research Center."April 1960."Cover title.Includes bibliographical references (p....

Chemical nonequilibrium effects on the inviscid flow in the windward plane of symmetry of two simplified shuttle configurations /

Lordi, John A.
Johnson, Charles B.
Vidal, Robert J.
Langley Research Center.

January 1973

Prepared at Langley Research Center.Cover title.Bibliography: p. 18-19.Mode of access: Internet

Static performance of an axisymmetric nozzle with post-exit vanes for multiaxis thrust vectoring /

Berrier, Bobby L.
Langley Research Center.

January 1988

Prepared at Langley Research Center."May 1988"--Cover.Includes bibliographical references (p. 11).Mo...

Experimental and analytical investigation of axisymmetric supersonic cruise nozzle geometry at Mach numbers form 0.60 to 1.30 /

Carson, George T.
Lee, Edwin E.
Langley Research Center.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.

January 1981

"December 1981"--Cover."Langley Research Center."Includes bibiliographical references.Mode of access...

Viscous-inviscid calculations of jet entrainment effects on the subsonic flow over nozzle afterbodies /

Wilmoth, Richard G.
Langley Research Center.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Office.

January 1980

Subject category 02."April 1980"--Cover."Langley Research Center."Includes bibliographical reference...

Effect of several geometric parameters on the static internal performance of three nonaxisymmetric nozzle concepts /

Berrier, Bobby L.
Re, Richard J.
Langley Research Center.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.

January 1979

Subject category 02.Includes statistical tables."July 1979"--Cover."Langley Research Center."Include...

Design of an axisymmetric, hypersonic nozzle, utilizing the method of characteristics

Bailey, Vincent Patrick, 1928-
Bailey, Vincent Patrick, 1928-

January 1962

This item was digitized from a paper original and/or a microfilm copy. If you need higher-resolution...

Static performance of nonaxisymmetric nozzles with yaw thrust-vectoring vanes /

Mason, Mary L.
Berrier, Bobby L.
Langley Research Center.

January 1988

Prepared at Langley Research Center."May 1988"--Cover.Includes bibliographical references (p. 10).Mo...

Effect of empennage arrangement on single-engine nozzle/afterbody static pressures at transonic speeds /

Henderson, William P.
Burley, James R.
Langley Research Center.

January 1987

Prepared at Langley Research Center."November 1987"--Cover.Includes bibliographical references (p. 7...

A preliminary assessment of the impact of 2-D exhaust-nozzle geometry on the cruise range of a hypersonic aircraft with top-mounted ramjet propulsion /

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

January 1980

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

A parametric study of effect of forebody shape on flow angularity at Mach 8 /

Johnson, Charles B.
Marcum, Don C.
Langley Research Center.

January 1974

Prepared at Langley Research Center.Cover title.Includes bibliographical references (p. 12-13).Mode ...

Hypersonic aerodynamic characteristics of a family of power-law, wing-body configuratioons /

Townsend, James C. (James Courtland), 1938-
Langley Research Center.

January 1973

Prepared at Langley Research Center.Cover title.Includes bibliographical references (p. 33-34).Mode ...

Effects of nozzle interfairing modifications on longitudinal aerodynamic characteristics of a twin-jet, variable-wing-sweep fighter model /

Reubush, David E.
Mercer, Charles E.
Langley Research Center.

January 1975

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

Investigation of Axisymmetric and nonaxisymmetric nozzels installed on a 0.10-scale F-18 protype airplane model /

Capone, Francis J.
Berrier, Bobby L.
Langley Research Center.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Office.

January 1980

"Subject Category 02.""Langley Research Center.""June 1980"--Cover.Includes bibliographical referenc...

Second-order small-disturbance solutions for hypersonic flow over power-law bodies /

Townsend, James C. (James Courtland), 1938-
Langley Research Center.

January 1975

Prepared at Langley Research Center.Cover title.Includes bibliographical references (p. 57-58).Mode ...

Effects of vibrational nonequilibrium on the inviscid design of an axisymmetric nozzle for hypersonic flow /

Abstract

Extracted data

Effects of vibrational nonequilibrium on the inviscid design of an axisymmetric nozzle for hypersonic flow /

Abstract

Extracted data

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