A transonic interactive boundary-layer theory for laminar and turbulent flow over swept wings /

Applicability of linearized-theory attached-flow methods to design and analysis of flap systems at low speeds for thin swept wings with sharp leading edges /

Carlson, Harry W.
Darden, Christine M.
Langley Research Center.

January 1987

Prepared at Langley Research Center."January 1987"--Cover.Includes bibliographical references (p. 14...

Computer program for calculating laminar and turbulent boundary layer development in compressible flow /

Herring, H. J.
Mellor, G. L.
Lewis Research Center.
Princeton University.

January 1972

"Prepared by Princeton University ... for Lewis Research Center."Cover title.Bibliography: p. 86-87....

A general method for calculating three-dimensional compressible laminar and turbulent boundary layers on arbitrary wings /

Cebeci, Tuncer.
Ramsey, Judy A., joint author.
Kaups, Kalle, joint author.
McDonnell Douglas Corporation.
Langley Research Center.
United States. National Aeronautics and Space Administration.

January 1977

Issued Jan. 1977.Prepared by McDonnell Douglas Corporation for Langley Research Center under NAS1-12...

A theoretical analysis of simulated transonic boundary layers in cryogenic-nitrogen wind tunnels /

Adcock, Jerry B.
Johnson, Charles B.
Langley Research Center.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Office.

January 1980

Subject Category 09."March 1980"--Cover."Langley Research Center."Includes bibliographical reference...

Forward-swept-wing configuration designed for high maneuverability by use of a transonic computational method /

Mann, Michael J.
Mercer, Charles E.
Langley Research Center.

January 1986

Prepared at Langley Research Center."November 1986"--Cover.Includes bibliographical references (p. 2...

Analysis of transonic flow about lifting wing-body configurations /

Barnwell, Richard W.
Langley Research Center.

January 1975

Prepared at Langley Research Center.Cover title.Includes bibliographical references (p. 69-71).Mode ...

The compressible turbulent boundary layer on a blunt swept slab with and without leading-edge blowing /

Hunt, James L. (James Larry), 1939-
Beckwith, Ivan E.
Bushnell, Dennis M.
Langley Research Center.
United States. National Aeronautics and Space Administration.

January 1971

Prepared at Langley Research Center."March 1971."Cover title.Includes bibliographical references (p....

The NASA Langley laminar-flow-control experiment on a swept, supercritical airfoil : design overview /

Harris, Charles D., 1952-
Brooks, Cuyler W.
Harvey, William D., 1934-
Langley Research Center.

Prepared at Langley Research Center."May 1988"--Cover.Includes bibliographical references (p. 22-24)...

A potential-flow/boundary layer method for calculating subsonic and transonic airfoil flow with trailing-edge separation /

Barnwell, Richard W.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.
Langley Research Center.

January 1981

Subject Category 02."Langley Research Center.""June 1981"--Cover.Includes bibliographical references...

Development of a nonlinear unsteady transonic flow theory /

Stahara, Stephen S.
Spreiter, John R.
Langley Research Center.
Nielsen Engineering & Research.

January 1973

"Prepared by Nielsen Engineering & Research, Inc. ... for Langley Research Center."Cover title.Bibli...

Lee-side flow over delta wings at supersonic speeds /

Miller, David S.
Wood, Richard M.
Langley Research Center.

January 1985

Prepared at Langley Research Center."June 1985"--Cover.Includes bibliographical references (p. 150)....

Supersonic aerodynamics of delta wings /

Wood, Richard M.
Langley Research Center.

January 1988

Prepared at Langley Research Center."March 1988"--Cover.Includes bibliographical references (p. 22-2...

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. ...

Flight-measured laminar boundary layer transition phenomena including stability theory analysis /

Obara, Clifford J.
Holmes, Bruce J.
Langley Research Center.

January 1985

Prepared at Langley Research Center."April 1985"--Cover.Includes bibliographical references (p. 8).M...

Aerodynamic characteristics of wings designed with a combined-theory method to cruise at a Mach number of 4.5 /

Mack, Robert J.
Langley Research Center.

January 1988

Prepared at Langley Research Center."April 1988"--Cover.Includes bibliographical references (p. 10-1...

Applicability of linearized-theory attached-flow methods to design and analysis of flap systems at low speeds for thin swept wings with sharp leading edges /

Carlson, Harry W.
Darden, Christine M.
Langley Research Center.

January 1987

Prepared at Langley Research Center."January 1987"--Cover.Includes bibliographical references (p. 14...

Computer program for calculating laminar and turbulent boundary layer development in compressible flow /

Herring, H. J.
Mellor, G. L.
Lewis Research Center.
Princeton University.

January 1972

"Prepared by Princeton University ... for Lewis Research Center."Cover title.Bibliography: p. 86-87....

A general method for calculating three-dimensional compressible laminar and turbulent boundary layers on arbitrary wings /

Cebeci, Tuncer.
Ramsey, Judy A., joint author.
Kaups, Kalle, joint author.
McDonnell Douglas Corporation.
Langley Research Center.
United States. National Aeronautics and Space Administration.

January 1977

Issued Jan. 1977.Prepared by McDonnell Douglas Corporation for Langley Research Center under NAS1-12...

A theoretical analysis of simulated transonic boundary layers in cryogenic-nitrogen wind tunnels /

Adcock, Jerry B.
Johnson, Charles B.
Langley Research Center.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Office.

January 1980

Subject Category 09."March 1980"--Cover."Langley Research Center."Includes bibliographical reference...

Forward-swept-wing configuration designed for high maneuverability by use of a transonic computational method /

Mann, Michael J.
Mercer, Charles E.
Langley Research Center.

January 1986

Prepared at Langley Research Center."November 1986"--Cover.Includes bibliographical references (p. 2...

Analysis of transonic flow about lifting wing-body configurations /

Barnwell, Richard W.
Langley Research Center.

January 1975

Prepared at Langley Research Center.Cover title.Includes bibliographical references (p. 69-71).Mode ...

The compressible turbulent boundary layer on a blunt swept slab with and without leading-edge blowing /

Hunt, James L. (James Larry), 1939-
Beckwith, Ivan E.
Bushnell, Dennis M.
Langley Research Center.
United States. National Aeronautics and Space Administration.

January 1971

Prepared at Langley Research Center."March 1971."Cover title.Includes bibliographical references (p....

The NASA Langley laminar-flow-control experiment on a swept, supercritical airfoil : design overview /

Harris, Charles D., 1952-
Brooks, Cuyler W.
Harvey, William D., 1934-
Langley Research Center.

Prepared at Langley Research Center."May 1988"--Cover.Includes bibliographical references (p. 22-24)...

A potential-flow/boundary layer method for calculating subsonic and transonic airfoil flow with trailing-edge separation /

Barnwell, Richard W.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.
Langley Research Center.

January 1981

Subject Category 02."Langley Research Center.""June 1981"--Cover.Includes bibliographical references...

Development of a nonlinear unsteady transonic flow theory /

Stahara, Stephen S.
Spreiter, John R.
Langley Research Center.
Nielsen Engineering & Research.

January 1973

"Prepared by Nielsen Engineering & Research, Inc. ... for Langley Research Center."Cover title.Bibli...

Lee-side flow over delta wings at supersonic speeds /

Miller, David S.
Wood, Richard M.
Langley Research Center.

January 1985

Prepared at Langley Research Center."June 1985"--Cover.Includes bibliographical references (p. 150)....

Supersonic aerodynamics of delta wings /

Wood, Richard M.
Langley Research Center.

January 1988

Prepared at Langley Research Center."March 1988"--Cover.Includes bibliographical references (p. 22-2...

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. ...

Flight-measured laminar boundary layer transition phenomena including stability theory analysis /

Obara, Clifford J.
Holmes, Bruce J.
Langley Research Center.

January 1985

Prepared at Langley Research Center."April 1985"--Cover.Includes bibliographical references (p. 8).M...

Aerodynamic characteristics of wings designed with a combined-theory method to cruise at a Mach number of 4.5 /

Mack, Robert J.
Langley Research Center.

January 1988

Prepared at Langley Research Center."April 1988"--Cover.Includes bibliographical references (p. 10-1...

Applicability of linearized-theory attached-flow methods to design and analysis of flap systems at low speeds for thin swept wings with sharp leading edges /

Carlson, Harry W.
Darden, Christine M.
Langley Research Center.

January 1987

Prepared at Langley Research Center."January 1987"--Cover.Includes bibliographical references (p. 14...

Computer program for calculating laminar and turbulent boundary layer development in compressible flow /

Herring, H. J.
Mellor, G. L.
Lewis Research Center.
Princeton University.

January 1972

"Prepared by Princeton University ... for Lewis Research Center."Cover title.Bibliography: p. 86-87....

A general method for calculating three-dimensional compressible laminar and turbulent boundary layers on arbitrary wings /

Cebeci, Tuncer.
Ramsey, Judy A., joint author.
Kaups, Kalle, joint author.
McDonnell Douglas Corporation.
Langley Research Center.
United States. National Aeronautics and Space Administration.

January 1977

Issued Jan. 1977.Prepared by McDonnell Douglas Corporation for Langley Research Center under NAS1-12...

A transonic interactive boundary-layer theory for laminar and turbulent flow over swept wings /

Abstract

Extracted data

A transonic interactive boundary-layer theory for laminar and turbulent flow over swept wings /

Abstract

Extracted data

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