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

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

Subsonic annular wing theory with application to flow about nacelles /

Mann, Michael J.
Langley Research Center.

January 1974

Prepared at Langley Research Center.Cover title.Includes bibliographical references (p. 90-91).Mode ...

An analysis of the crossover between local and massive separation on airfoils /

Burnett, M.
Carter, J. E.
Langley Research Center.

January 1987

"September 1987"--Cover."Prepared for Langley Research Center under Contract NAS1-16585."Includes bi...

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....

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...

A computational model for the prediction of jet entrainment in the vicinity of nozzle boattails (The BOAT code) /

Dash, Sanford M.
Pergament, Harold S., joint author.
Aeronautical Research Associates of Princeton.
Langley Research Center.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Office.

January 1978

Dec. 1978.Contract NAS1-14794.Includes bibliographical references.Mode of access: Internet

An Improved interaction method for calculating exhaust nozzle boattail flows /

Kuhn, Gary D.. author.
United States. Air Force. Arnold Air Force Base. sponsor.
Arnold Engineering Development Center. sponsor.
Nielsen Engineering & Research. issuing body.

"Final Report, September 1978--December 1979.""Program Element 65807F.""October 1980."Includes bibli...

Investigation at supersonic speeds of the variation with Reynolds number and Mach number of the total, base, and skin-friction drag of seven boattail bodies of revolution designed for minimum wave drag /

Bromm, August F.
Goodwin, Julia M.
Langley Aeronautical Laboratory.
United States. National Adviosry Committee for Aeronautics. NACA research memorandum.

January 1953

"December 1, 1953."Includes bibliographical references (p. 10).Mode of access: Internet

Effect of a trade between boattail angle and wedge size on the performance of a nonaxisymmetric wedge nozzle /

Carson, George T.
Burley, James R.
Bare, E. Ann.
Langley Research Center.

January 1987

Prepared at Langley Research Center."July 1987"--Cover.Includes bibliographical references (p. 7-8)....

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...

Fuselage and nozzle pressure distributions on a 1/12-scale F-15 propulsion model at transonic speeds /

Pendergraft, Odis C.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.
Langley Research Center.

January 1979

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

Fundamental studies of subsonic and transonic flow separation.

Wu, J. M., author
United States. Air Force. Systems Command. Arnold Engineering Development Center. sponsor.
University of Tennessee (System). Space Institute. issuing body.

"Program Element 65807F.""Final Report--November 1975--September 1978.""October 1979."Includes bibli...

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

Investigation of convergent-divergent nozzles applicable to reduced-power supersonic cruise aircraft /

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

January 1980

Dec. 1980."Langely Research Center."Includes bibliographical references.Mode of access: Internet

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

King, R. W.
Buteau, J. D.
Presz, W. M., Jr.

July 1978

A practical engineering calculation was developed to model the viscous effects of a separated, rever...

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

Subsonic annular wing theory with application to flow about nacelles /

Mann, Michael J.
Langley Research Center.

January 1974

Prepared at Langley Research Center.Cover title.Includes bibliographical references (p. 90-91).Mode ...

An analysis of the crossover between local and massive separation on airfoils /

Burnett, M.
Carter, J. E.
Langley Research Center.

January 1987

"September 1987"--Cover."Prepared for Langley Research Center under Contract NAS1-16585."Includes bi...

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....

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...

A computational model for the prediction of jet entrainment in the vicinity of nozzle boattails (The BOAT code) /

Dash, Sanford M.
Pergament, Harold S., joint author.
Aeronautical Research Associates of Princeton.
Langley Research Center.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Office.

January 1978

Dec. 1978.Contract NAS1-14794.Includes bibliographical references.Mode of access: Internet

An Improved interaction method for calculating exhaust nozzle boattail flows /

Kuhn, Gary D.. author.
United States. Air Force. Arnold Air Force Base. sponsor.
Arnold Engineering Development Center. sponsor.
Nielsen Engineering & Research. issuing body.

"Final Report, September 1978--December 1979.""Program Element 65807F.""October 1980."Includes bibli...

Investigation at supersonic speeds of the variation with Reynolds number and Mach number of the total, base, and skin-friction drag of seven boattail bodies of revolution designed for minimum wave drag /

Bromm, August F.
Goodwin, Julia M.
Langley Aeronautical Laboratory.
United States. National Adviosry Committee for Aeronautics. NACA research memorandum.

January 1953

"December 1, 1953."Includes bibliographical references (p. 10).Mode of access: Internet

Effect of a trade between boattail angle and wedge size on the performance of a nonaxisymmetric wedge nozzle /

Carson, George T.
Burley, James R.
Bare, E. Ann.
Langley Research Center.

January 1987

Prepared at Langley Research Center."July 1987"--Cover.Includes bibliographical references (p. 7-8)....

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...

Fuselage and nozzle pressure distributions on a 1/12-scale F-15 propulsion model at transonic speeds /

Pendergraft, Odis C.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.
Langley Research Center.

January 1979

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

Fundamental studies of subsonic and transonic flow separation.

Wu, J. M., author
United States. Air Force. Systems Command. Arnold Engineering Development Center. sponsor.
University of Tennessee (System). Space Institute. issuing body.

"Program Element 65807F.""Final Report--November 1975--September 1978.""October 1979."Includes bibli...

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

Investigation of convergent-divergent nozzles applicable to reduced-power supersonic cruise aircraft /

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

January 1980

Dec. 1980."Langely Research Center."Includes bibliographical references.Mode of access: Internet

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

King, R. W.
Buteau, J. D.
Presz, W. M., Jr.

July 1978

A practical engineering calculation was developed to model the viscous effects of a separated, rever...

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

Subsonic annular wing theory with application to flow about nacelles /

Mann, Michael J.
Langley Research Center.

January 1974

Prepared at Langley Research Center.Cover title.Includes bibliographical references (p. 90-91).Mode ...

An analysis of the crossover between local and massive separation on airfoils /

Burnett, M.
Carter, J. E.
Langley Research Center.

January 1987

"September 1987"--Cover."Prepared for Langley Research Center under Contract NAS1-16585."Includes bi...

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

Abstract

Extracted data

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

Abstract

Extracted data

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