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

Dispersion of turbojet engine exhaust in flight /

Holdeman, James D.
Lewis Research Center.

January 1973

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

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 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...

Effect of Reynolds number on the subsonic boattail drag of several wing-body configurations /

Reubush, David E.
United States. National Aeronautics and Space Administration.
Langley Research Center.

January 1976

Cover title.Includes bibliographical references (p. 8-9).Mode of access: Internet

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....

Numerical calculation of transonic boattail flow /

Chow, Wen L.
Anderson, Bernhard H.
Bober, Lawrence J.
Lewis Research Center.

January 1975

Prepared at Lewis Research Center.Cover title.Includes bibliographical references (p. 16).Mode of ac...

Flight investigation of installation effects on a plug nozzle with a series of boattailed primary shrouds installed on an underwing nacelle /

Head, Verlon L.
Lewis Research Center.

January 1974

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

Calculation of the pressure distribution on axisymmetric boattails including effects of viscous interactions and exhaust jets in subsonic flow /

Rom, Josef, 1932-
Bober, Lawrence J.
Lewis Research Center.

January 1974

Prepared at Lewis Research Center.Cover title.Includes bibliographical references (p. 11-12).Mode of...

Flight velocity effects on the jet noise of several variations of a 104-tube suppressor nozzle /

Burley, Richard R.
Lewis Research Center.

January 1974

Prepared at Lewis Research Center.Cover title.Includes bibliographical references (p. 23-24).Mode of...

Experimental study of the effectiveness of cylindrical plume simulators for predicting jet-on boattail drag at Mach numberes up to 1.30 /

Reubush, David E.
Lanlgely Research Center.

January 1974

Prepared at Langley Research Center.Cover title.Includes bibliographical references (p. 17-19).Mode ...

Effect of fineness ratio on boattail drag of circular-arc afterbodies having closure ratios of 0.50 with jet exhaust at Mach numbers up to 1.30 /

Reubush, David E.
Runckel, Jack F.
Langley Research Center.

January 1973

Prepared at Langley Research Center.Cover title.Bibliography: p. 20-21.Mode of access: Internet

An improved analytical model of the separation region on boattail nozzles at subsonic speeds /

Presz, Walter M.
Buteau, John D., joint author.
King, Ronald W., joint author.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Office.

January 1978

Issued July 1978.Prepared for Langley Research Center, by United Technologies Corporation, under con...

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

Chamberlin, R.

May 1974

A contoured boattail nozzle typical of those used on a twin-engine fighter was tested on an underwin...

Flight investigation of installation effects on a wedge nozzle installed on an underwing nacelle /

Johns, Albert L.
Lewis Research Center.

January 1975

Prepared at Lewis Research Center.Cover title.Includes bibliographical references (p. 14-15).Mode of...

Effects of Mach number on pitot-probe displacment in a turbulent boundary layer /

Allen, Jerry M.
Langley Research Center.

January 1974

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

Dispersion of turbojet engine exhaust in flight /

Holdeman, James D.
Lewis Research Center.

January 1973

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

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 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...

Effect of Reynolds number on the subsonic boattail drag of several wing-body configurations /

Reubush, David E.
United States. National Aeronautics and Space Administration.
Langley Research Center.

January 1976

Cover title.Includes bibliographical references (p. 8-9).Mode of access: Internet

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....

Numerical calculation of transonic boattail flow /

Chow, Wen L.
Anderson, Bernhard H.
Bober, Lawrence J.
Lewis Research Center.

January 1975

Prepared at Lewis Research Center.Cover title.Includes bibliographical references (p. 16).Mode of ac...

Flight investigation of installation effects on a plug nozzle with a series of boattailed primary shrouds installed on an underwing nacelle /

Head, Verlon L.
Lewis Research Center.

January 1974

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

Calculation of the pressure distribution on axisymmetric boattails including effects of viscous interactions and exhaust jets in subsonic flow /

Rom, Josef, 1932-
Bober, Lawrence J.
Lewis Research Center.

January 1974

Prepared at Lewis Research Center.Cover title.Includes bibliographical references (p. 11-12).Mode of...

Flight velocity effects on the jet noise of several variations of a 104-tube suppressor nozzle /

Burley, Richard R.
Lewis Research Center.

January 1974

Prepared at Lewis Research Center.Cover title.Includes bibliographical references (p. 23-24).Mode of...

Experimental study of the effectiveness of cylindrical plume simulators for predicting jet-on boattail drag at Mach numberes up to 1.30 /

Reubush, David E.
Lanlgely Research Center.

January 1974

Prepared at Langley Research Center.Cover title.Includes bibliographical references (p. 17-19).Mode ...

Effect of fineness ratio on boattail drag of circular-arc afterbodies having closure ratios of 0.50 with jet exhaust at Mach numbers up to 1.30 /

Reubush, David E.
Runckel, Jack F.
Langley Research Center.

January 1973

Prepared at Langley Research Center.Cover title.Bibliography: p. 20-21.Mode of access: Internet

An improved analytical model of the separation region on boattail nozzles at subsonic speeds /

Presz, Walter M.
Buteau, John D., joint author.
King, Ronald W., joint author.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Office.

January 1978

Issued July 1978.Prepared for Langley Research Center, by United Technologies Corporation, under con...

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

Chamberlin, R.

May 1974

A contoured boattail nozzle typical of those used on a twin-engine fighter was tested on an underwin...

Flight investigation of installation effects on a wedge nozzle installed on an underwing nacelle /

Johns, Albert L.
Lewis Research Center.

January 1975

Prepared at Lewis Research Center.Cover title.Includes bibliographical references (p. 14-15).Mode of...

Effects of Mach number on pitot-probe displacment in a turbulent boundary layer /

Allen, Jerry M.
Langley Research Center.

January 1974

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

Dispersion of turbojet engine exhaust in flight /

Holdeman, James D.
Lewis Research Center.

January 1973

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

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 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...

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

Abstract

Extracted data

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

Abstract

Extracted data

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