A viscous flow analysis for the tip vortex generation process /

Effect of inlet ingestion of a wing tip vortex on compressor face flow and turbojet stall margin /

Mitchell, Glenn A.
Lewis Research Center.

January 1975

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

Aerodynamic performance of axial-flow fan stage operated at nine inlet guide vane angles /

Moore, Royce D.
Reid, Lonnie.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.

January 1979

"September 1979"--Cover.Includes bibliographical references (p. 12).Mode of access: Internet

Sensitivity of F-106B leading-edge-vortex images to flight and vapor-screen parameters /

Lamar, John E.
Johnson, Thomas D.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Division.

January 1988

"June 1988"--Cover.Includes bibliographical references (p. 11).Mode of access: Internet

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

Viscous analysis of three-dimensional rotor flows using a multigrid method /

Arnone, A.
United States. National Aeronautics and Space Administration.

January 1993

"July 1993."Cover title.Includes bibliographical references (p. 19-21).Mode of access: Internet

Hypersonic viscous drag on cones in rarefied flow /

Kussoy, M. I. (Marvin I.)
Ames Research Center.
United States. National Aeronautics and Space Administration.

January 1967

Cover title."June 1967."Includes bibliographical references (p. 11-12).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...

Transonic flow analysis for rotors.

Chang, I-Chung.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Division.

January 1990

"June 1990."Cover title.Distributed to depository libraries in microfiche.Includes bibliographical r...

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. ...

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...

Development of a three-dimensional supersonic inlet flow analysis /

Buggeln, R. C.
Lewis Research Center.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Office.

January 1980

"January 1980"--Cover.Includes bibliographical references.Mode of access: Internet

Semianalytic modeling of aerodynamic shapes /

Barger, Raymond L.
Adams, Mary S.
Langley Research Center.

January 1985

Prepared at Langley Research Center."April 1985"--Cover.Includes bibliographical references (p. 6).M...

Vortex flow and erosion in rocket nozzles due to warm-gas injection for thrust vector control /

Smith, G. Louis.
United States. National Aeronautics and Space Administration.

Cover title."February 1966."Includes bibliographical references.Mode of access: Internet

Computer analysis of flow pertubations generated by placement of choke bumps in a wind tunnel /

Campbell, Richard L. (Richard Lawson), 1952-
Langley Research Center.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.

January 1981

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

The disturbance flow field produced by an evolving vortex /

Gatski, T. B.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.

January 1983

Subject category 34."December 1983"--Cover.Distributed to depository libraries in microfiche.Include...

Effect of inlet ingestion of a wing tip vortex on compressor face flow and turbojet stall margin /

Mitchell, Glenn A.
Lewis Research Center.

January 1975

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

Aerodynamic performance of axial-flow fan stage operated at nine inlet guide vane angles /

Moore, Royce D.
Reid, Lonnie.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.

January 1979

"September 1979"--Cover.Includes bibliographical references (p. 12).Mode of access: Internet

Sensitivity of F-106B leading-edge-vortex images to flight and vapor-screen parameters /

Lamar, John E.
Johnson, Thomas D.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Division.

January 1988

"June 1988"--Cover.Includes bibliographical references (p. 11).Mode of access: Internet

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

Viscous analysis of three-dimensional rotor flows using a multigrid method /

Arnone, A.
United States. National Aeronautics and Space Administration.

January 1993

"July 1993."Cover title.Includes bibliographical references (p. 19-21).Mode of access: Internet

Hypersonic viscous drag on cones in rarefied flow /

Kussoy, M. I. (Marvin I.)
Ames Research Center.
United States. National Aeronautics and Space Administration.

January 1967

Cover title."June 1967."Includes bibliographical references (p. 11-12).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...

Transonic flow analysis for rotors.

Chang, I-Chung.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Division.

January 1990

"June 1990."Cover title.Distributed to depository libraries in microfiche.Includes bibliographical r...

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. ...

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...

Development of a three-dimensional supersonic inlet flow analysis /

Buggeln, R. C.
Lewis Research Center.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Office.

January 1980

"January 1980"--Cover.Includes bibliographical references.Mode of access: Internet

Semianalytic modeling of aerodynamic shapes /

Barger, Raymond L.
Adams, Mary S.
Langley Research Center.

January 1985

Prepared at Langley Research Center."April 1985"--Cover.Includes bibliographical references (p. 6).M...

Vortex flow and erosion in rocket nozzles due to warm-gas injection for thrust vector control /

Smith, G. Louis.
United States. National Aeronautics and Space Administration.

Cover title."February 1966."Includes bibliographical references.Mode of access: Internet

Computer analysis of flow pertubations generated by placement of choke bumps in a wind tunnel /

Campbell, Richard L. (Richard Lawson), 1952-
Langley Research Center.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.

January 1981

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

The disturbance flow field produced by an evolving vortex /

Gatski, T. B.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.

January 1983

Subject category 34."December 1983"--Cover.Distributed to depository libraries in microfiche.Include...

Effect of inlet ingestion of a wing tip vortex on compressor face flow and turbojet stall margin /

Mitchell, Glenn A.
Lewis Research Center.

January 1975

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

Aerodynamic performance of axial-flow fan stage operated at nine inlet guide vane angles /

Moore, Royce D.
Reid, Lonnie.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.

January 1979

"September 1979"--Cover.Includes bibliographical references (p. 12).Mode of access: Internet

Sensitivity of F-106B leading-edge-vortex images to flight and vapor-screen parameters /

Lamar, John E.
Johnson, Thomas D.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Division.

January 1988

"June 1988"--Cover.Includes bibliographical references (p. 11).Mode of access: Internet

A viscous flow analysis for the tip vortex generation process /

Abstract

Extracted data

A viscous flow analysis for the tip vortex generation process /

Abstract

Extracted data

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