Numerical study of axisymmetric vortex breakdowns /

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...

Decay of far flow field in trailing vortices /

Baldwin, Barrett S. (Barrett Stone)
Sheaffer, Yvonne S.
Chigier, N. A.
Ames Research Center.

January 1974

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

Vortex calculations using extended potential flow theory /

Guyton, Robert W., author.
Wright Research and Development Center, sponsor.
Air Force Flight Dynamics Laboratory (U.S.), sponsor.
United States. Air Force. Systems Command, issuing body.

"July 1989."Includes bibliographical references (page 9).Print reproduction.Mode of access: Internet

Vortex equations : singularities, numerical solution, and axisymmetric vortex breakdown /

Bossel, Hartmut H. (Helmut Hans)
Langley Research Center.
University of California, Santa Barbara.

January 1972

"Prepared by University of California, Santa Barbara ... for Langley Research Center."Cover title.Bi...

Vortex shedding from a blunt trailing edge with equal and unequal external mean velocities /

Brinich, Paul F.
Goldstein, Marvin E.
Boldman, Donald R.
Lewis Research Center.

January 1975

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

Performance of vortex generators in a Mach 2.5 low-bleed full-scale 45-percent-internal-contraction axisymmetric inlet /

Neumann, Harvey E.
Shaw, Robert J. (Robert Joseph), 1946-
Wasserbauer, Joseph F.
Lewis Research Center.

January 1975

Prepared at Lewis Research Center.Cover title.Includes bibliographical references (p. 17).Mode of ac...

The vortex lattice method for the rotor-vortex interaction problem /

Padakannaya, Raghuveera.
Langley Research Center.
Pennsylvania State University.

January 1974

"Prepared by the Pennsylvania State University ... for Langley Research Center. "Cover title.Include...

An experimental study of rotor blade-vortex interaction /

Surendraiah, Makam.
United States. National Aeronautics and Space Administration.
Langley Research Center.
Pennsylvania State University.

January 1970

Prepared by Pennsylvania State University for Langley Research Center."N70-25692."Includes bibliogra...

Performance of centerbody vortex generators in an axisymmetric mixed-compression inlet at Mach numbers from 2.0 to 3.0 /

Mitchell, Glen A.
Davis, Ronald W.
Lewis Research Center.
United States. National Aeronautics and Space Administration.

January 1968

Cover title."July 1968."Includes bibliographical references (p. 12).Mode of access: Internet

Stability of a plane vortex sheet between gases exchanging heat by radiation /

Eno, Burton E.
Cornell University.
Lewis Research Center.
United States. National Aeronautics and Space Administration.

January 1971

Prepared by Cornell University for Lewis Research Center.N71-35411.Mode of access: Internet

Simulator study of vortex encounters by a twin-engine, commercial, jet transport airplane /

Hastings, Earl C.
Keyser, Gerald L.
Langley Research Center.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.

January 1982

Subject category 08."February 1982"--Cover.Includes bibliographical references.Mode of access: Inter...

A theoretical method for the analysis and design of axisymmetric bodies /

Beatty, T. D.
Langley Research Center.
McDonnell Douglas Corporation.

January 1975

Prepared at McDonnell Douglas Aircraft Corporation for Langley Research Center under Contract NAS1-1...

Finite-difference solution for turbulent swirling compressible flow in axisymmetric ducts with struts /

Anderson, O. L. (Olos Lennart), 1931-
Lewis Research Center.
United Aircraft Corporation.

January 1974

"Prepared by United Aircraft Corporation ... for Lewis Research Center."Cover title.Bibliography: p....

A viscous flow analysis for the tip vortex generation process /

Shamroth, S.J.
Briley, W. R.
Langley Research Center.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.

January 1979

"October 1979"--Cover.Includes bibliographical references.Mode of access: Internet

An experimental investigation of vortex generation in a turbulent boundary layer undergoing adverse pressure gradient /

Zakkay, Victor.
Calarese, Wladimiro.
Langley Research Center.
New York University.

January 1972

"Prepared by New York University ... for Langley Research Center."Cover title.Bibliography: p. 9.Mod...

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...

Decay of far flow field in trailing vortices /

Baldwin, Barrett S. (Barrett Stone)
Sheaffer, Yvonne S.
Chigier, N. A.
Ames Research Center.

January 1974

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

Vortex calculations using extended potential flow theory /

Guyton, Robert W., author.
Wright Research and Development Center, sponsor.
Air Force Flight Dynamics Laboratory (U.S.), sponsor.
United States. Air Force. Systems Command, issuing body.

"July 1989."Includes bibliographical references (page 9).Print reproduction.Mode of access: Internet

Vortex equations : singularities, numerical solution, and axisymmetric vortex breakdown /

Bossel, Hartmut H. (Helmut Hans)
Langley Research Center.
University of California, Santa Barbara.

January 1972

"Prepared by University of California, Santa Barbara ... for Langley Research Center."Cover title.Bi...

Vortex shedding from a blunt trailing edge with equal and unequal external mean velocities /

Brinich, Paul F.
Goldstein, Marvin E.
Boldman, Donald R.
Lewis Research Center.

January 1975

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

Performance of vortex generators in a Mach 2.5 low-bleed full-scale 45-percent-internal-contraction axisymmetric inlet /

Neumann, Harvey E.
Shaw, Robert J. (Robert Joseph), 1946-
Wasserbauer, Joseph F.
Lewis Research Center.

January 1975

Prepared at Lewis Research Center.Cover title.Includes bibliographical references (p. 17).Mode of ac...

The vortex lattice method for the rotor-vortex interaction problem /

Padakannaya, Raghuveera.
Langley Research Center.
Pennsylvania State University.

January 1974

"Prepared by the Pennsylvania State University ... for Langley Research Center. "Cover title.Include...

An experimental study of rotor blade-vortex interaction /

Surendraiah, Makam.
United States. National Aeronautics and Space Administration.
Langley Research Center.
Pennsylvania State University.

January 1970

Prepared by Pennsylvania State University for Langley Research Center."N70-25692."Includes bibliogra...

Performance of centerbody vortex generators in an axisymmetric mixed-compression inlet at Mach numbers from 2.0 to 3.0 /

Mitchell, Glen A.
Davis, Ronald W.
Lewis Research Center.
United States. National Aeronautics and Space Administration.

January 1968

Cover title."July 1968."Includes bibliographical references (p. 12).Mode of access: Internet

Stability of a plane vortex sheet between gases exchanging heat by radiation /

Eno, Burton E.
Cornell University.
Lewis Research Center.
United States. National Aeronautics and Space Administration.

January 1971

Prepared by Cornell University for Lewis Research Center.N71-35411.Mode of access: Internet

Simulator study of vortex encounters by a twin-engine, commercial, jet transport airplane /

Hastings, Earl C.
Keyser, Gerald L.
Langley Research Center.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.

January 1982

Subject category 08."February 1982"--Cover.Includes bibliographical references.Mode of access: Inter...

A theoretical method for the analysis and design of axisymmetric bodies /

Beatty, T. D.
Langley Research Center.
McDonnell Douglas Corporation.

January 1975

Prepared at McDonnell Douglas Aircraft Corporation for Langley Research Center under Contract NAS1-1...

Finite-difference solution for turbulent swirling compressible flow in axisymmetric ducts with struts /

Anderson, O. L. (Olos Lennart), 1931-
Lewis Research Center.
United Aircraft Corporation.

January 1974

"Prepared by United Aircraft Corporation ... for Lewis Research Center."Cover title.Bibliography: p....

A viscous flow analysis for the tip vortex generation process /

Shamroth, S.J.
Briley, W. R.
Langley Research Center.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.

January 1979

"October 1979"--Cover.Includes bibliographical references.Mode of access: Internet

An experimental investigation of vortex generation in a turbulent boundary layer undergoing adverse pressure gradient /

Zakkay, Victor.
Calarese, Wladimiro.
Langley Research Center.
New York University.

January 1972

"Prepared by New York University ... for Langley Research Center."Cover title.Bibliography: p. 9.Mod...

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...

Decay of far flow field in trailing vortices /

Baldwin, Barrett S. (Barrett Stone)
Sheaffer, Yvonne S.
Chigier, N. A.
Ames Research Center.

January 1974

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

Vortex calculations using extended potential flow theory /

Guyton, Robert W., author.
Wright Research and Development Center, sponsor.
Air Force Flight Dynamics Laboratory (U.S.), sponsor.
United States. Air Force. Systems Command, issuing body.

"July 1989."Includes bibliographical references (page 9).Print reproduction.Mode of access: Internet

Numerical study of axisymmetric vortex breakdowns /

Abstract

Extracted data

Numerical study of axisymmetric vortex breakdowns /

Abstract

Extracted data

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