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

Flight Reynolds number effects on a contoured boattail nozzle at subsonic speeds /

Chamberlin, Roger.
Lewis Research Center.

January 1974

Prepared at Lewis Research Center.Cover title.Includes bibliographical references (p. 8-9).Mode of a...

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

Anders, John Benjamin.
Langley Research Center.

January 1975

Prepared at Langley Research Center.Cover title.Includes bibliographical references (p. 20-22).Mode ...

Görtler vortices and transition in wall boundary layers of two Mach 5 nozzles /

Beckwith, Ivan E.
Holley, Barbara B.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.
Langley Research Center.

January 1981

"August 1981"--Cover."Langley Research Center."Includes bibliographical references.Mode of access: I...

Jet effects on cylindrical afterbodies housing sonic and supersonic nozzles which exhaust against a supersonic stream at angles of attack from 90 ̊to 180 ̊/

Hayman, Lovick O.
McDearmon, Russell W.
Langley Research Center.

Prepared at Langley Research Center."March 1962."Cover title.Includes bibliographical references (p....

Calculation of viscous effects on transonic flow for oscillating airfoils and comparisons with experiment /

Howlett, James T.
Bland, Samuel R.
Langley Research Center.

January 1987

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

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...

Multiscale turbulence effects in supersonic jets exhausting into still air /

Abdol-Hamid, Khaled S. (Khaled Sayed), 1957-
Wilmoth, Richard G.
Langley Research Center.

January 1987

Prepared at Langley Research Center."July 1987"--Cover.Includes bibliographical references (p. 11).M...

An analytical study of the effects of jets located more than one jet diameter above a wing at subsonic speeds /

Putnam, Lawrence E. (Lawrence Elwood)
Langley Research Center.

January 1974

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

Theoretical and experimental flow fields for a supersonic cruise fighter forebody /

Yaros, Steven F.
Langley Research Center.

January 1985

Prepared at Langley Research Center."November 1984"--Cover.Includes bibliographical references (p. 7...

Investigations of a flow field surrounding circular-arc boattail nozzles at subsonic speeds /

Abeyounis, William Kelly.
Putnam, Lawrence E. (Lawrence Ellwood)
Langley Research Center.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Office.

January 1980

Subject Category 02."May 1980"--Cover."Langley Research Center."Includes bibliographical references....

Jet effects at supersonic speeds on base and afterbody pressures of a missile model having single and multiple jets /

Charczenko, Nickolai.
Hayes, Clyde.
Langley Research Center.

Prepared at Langley Research Center."November 1963"--Cover.Includes bibliographical references (p. 8...

Viscous computations of cold air/air flow around scramjet nozzle afterbody /

Baysal, Oktay.
Englelund, Walter C.
Old Dominion University. Dept. of Mechanical Engineering and Mechanics.
Langley Research Center.

January 1991

Prepared at the Mechanical Engineering & Mechanics Dept., Old Dominion University, for Langley Resea...

Effect of several airframe/nozzle modifications on the drag of a variable-sweep bomber configuration /

Re, Richard J.
Reubush, David E.
Langley Research Center.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.

January 1979

"October 1979"--Cover."Langley Research Center."Includes bibliographical references.Mode of access: ...

The effect of thrust minus base drag of exchanging base area for nozzle expansion in supersonic nozzles at transonic mach numbers /

Slocumb, Travis H.
Andrews, Earl H.
United States. National Aeronautics and Space Administration.

Cover title."April 1961."Aerodynamics, aircraft; Aerodynamics, missiles and space vehicles; Aircraft...

Numerical study of sound propagation in a jet flow /

Padula, Sharon L.
Liu, Chen-Huei.
Langley Research Center.

January 1975

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

Flight Reynolds number effects on a contoured boattail nozzle at subsonic speeds /

Chamberlin, Roger.
Lewis Research Center.

January 1974

Prepared at Lewis Research Center.Cover title.Includes bibliographical references (p. 8-9).Mode of a...

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

Anders, John Benjamin.
Langley Research Center.

January 1975

Prepared at Langley Research Center.Cover title.Includes bibliographical references (p. 20-22).Mode ...

Görtler vortices and transition in wall boundary layers of two Mach 5 nozzles /

Beckwith, Ivan E.
Holley, Barbara B.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.
Langley Research Center.

January 1981

"August 1981"--Cover."Langley Research Center."Includes bibliographical references.Mode of access: I...

Jet effects on cylindrical afterbodies housing sonic and supersonic nozzles which exhaust against a supersonic stream at angles of attack from 90 ̊to 180 ̊/

Hayman, Lovick O.
McDearmon, Russell W.
Langley Research Center.

Prepared at Langley Research Center."March 1962."Cover title.Includes bibliographical references (p....

Calculation of viscous effects on transonic flow for oscillating airfoils and comparisons with experiment /

Howlett, James T.
Bland, Samuel R.
Langley Research Center.

January 1987

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

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...

Multiscale turbulence effects in supersonic jets exhausting into still air /

Abdol-Hamid, Khaled S. (Khaled Sayed), 1957-
Wilmoth, Richard G.
Langley Research Center.

January 1987

Prepared at Langley Research Center."July 1987"--Cover.Includes bibliographical references (p. 11).M...

An analytical study of the effects of jets located more than one jet diameter above a wing at subsonic speeds /

Putnam, Lawrence E. (Lawrence Elwood)
Langley Research Center.

January 1974

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

Theoretical and experimental flow fields for a supersonic cruise fighter forebody /

Yaros, Steven F.
Langley Research Center.

January 1985

Prepared at Langley Research Center."November 1984"--Cover.Includes bibliographical references (p. 7...

Investigations of a flow field surrounding circular-arc boattail nozzles at subsonic speeds /

Abeyounis, William Kelly.
Putnam, Lawrence E. (Lawrence Ellwood)
Langley Research Center.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Office.

January 1980

Subject Category 02."May 1980"--Cover."Langley Research Center."Includes bibliographical references....

Jet effects at supersonic speeds on base and afterbody pressures of a missile model having single and multiple jets /

Charczenko, Nickolai.
Hayes, Clyde.
Langley Research Center.

Prepared at Langley Research Center."November 1963"--Cover.Includes bibliographical references (p. 8...

Viscous computations of cold air/air flow around scramjet nozzle afterbody /

Baysal, Oktay.
Englelund, Walter C.
Old Dominion University. Dept. of Mechanical Engineering and Mechanics.
Langley Research Center.

January 1991

Prepared at the Mechanical Engineering & Mechanics Dept., Old Dominion University, for Langley Resea...

Effect of several airframe/nozzle modifications on the drag of a variable-sweep bomber configuration /

Re, Richard J.
Reubush, David E.
Langley Research Center.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.

January 1979

"October 1979"--Cover."Langley Research Center."Includes bibliographical references.Mode of access: ...

The effect of thrust minus base drag of exchanging base area for nozzle expansion in supersonic nozzles at transonic mach numbers /

Slocumb, Travis H.
Andrews, Earl H.
United States. National Aeronautics and Space Administration.

Cover title."April 1961."Aerodynamics, aircraft; Aerodynamics, missiles and space vehicles; Aircraft...

Numerical study of sound propagation in a jet flow /

Padula, Sharon L.
Liu, Chen-Huei.
Langley Research Center.

January 1975

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

Flight Reynolds number effects on a contoured boattail nozzle at subsonic speeds /

Chamberlin, Roger.
Lewis Research Center.

January 1974

Prepared at Lewis Research Center.Cover title.Includes bibliographical references (p. 8-9).Mode of a...

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

Anders, John Benjamin.
Langley Research Center.

January 1975

Prepared at Langley Research Center.Cover title.Includes bibliographical references (p. 20-22).Mode ...

Görtler vortices and transition in wall boundary layers of two Mach 5 nozzles /

Beckwith, Ivan E.
Holley, Barbara B.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.
Langley Research Center.

January 1981

"August 1981"--Cover."Langley Research Center."Includes bibliographical references.Mode of access: I...

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

Abstract

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

Abstract

Extracted data

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