Computation of the transonic perturbation flow fields around two- and three-dimensional oscillating wings /

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...

Calculation of the twist distribution of wings designed for cruise at transonic speeds /

Mann, Michael J.
Langley Research Center.

January 1974

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

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

Woodson, Shawn H.
DeJarnette, Fred R.
Langley Research Center.

January 1988

"October 1988"--Cover."Prepared for Langley Research Center under Cooperative Agreement NCC1-22."Inc...

A finite difference method for the solution of the transonic flow around harmonically oscillating wings /

Ehlers, F. Edward.
Langley Research Center.
Boeing Commercial Airplane Company.

January 1974

"Prepared by Boeing Commercial Aircraft Company ... for Langley Research Center."Cover title.Bibliog...

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. ...

Calculative techniques for transonic flows about certain classes of wing-body combinations /

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

January 1972

"Prepared by Nielsen Engineering & Research, Inc. ... for Ames Research Center."Cover title.Bibliogr...

The practical application of a finite difference method for analyzing transonic flow over oscillating airfoils and wings /

Ehlers, F. Edward, joint author.
Sebastian, James D., joint author.
Boeing Commercial Airplane Company.
Langley Research Center.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Office.

January 1978

Issued Feb. 1978.Prepared for Langley Research Center under Contact NAS 1-14204.Includes bibliograph...

Flow field analysis of aircraft configurations using a numerical solution to the three-dimensional unified supersonic/hypersonic small disturbance equations /

Gunness, R. C.
Dsylva, E.
Knight, C. J.
Langley Research Center.
Boeing Company.

January 1972

"February 1972."Cover title.Performed by the Boeing Company, Seattle, Wash., for Langley Research C...

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 ...

Computation of transonic potential flow about three-dimensional inlets, ducts, and bodies /

Reyhner, Theodore A.
Boeing Commercial Airplane Company.
Langley Research Center.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.

January 1982

Subject Category 02."March 1982"--Cover.Includes bibliographical references.Mode of access: Internet

Computation of the transonic perturbation flow fields around two- and three-dimensional oscillating wings

Weatherill, W. H.
Ehlers, F. E.
Sebastian, J. D.

December 1975

Analytical and empirical studies of a finite difference method for the solution of the transonic flo...

Calculation of the longitudinal aerodynamic characteristics of wing-flap configurations with externally blown flaps /

Mendenhall, M. R.
Langley Research Center.
Nielsen Engineering & Research.

"Prepared by Nielsen Engineering & Research, Inc. ... for Langley Research Center.""September 1976."...

Contribution to methods for calculating the flow about thin lifting wings at transonic speeds : Analytic expressions for the far field /

Klunker, E. B.
United States. National Aeronautics and Space Administration.
Langley Research Center.

January 1971

Prepared at Langley Research Center.N72-11289.Cover title.Includes bibliographical references (p. 15...

Calculation of three-dimensional unsteady transonic flows past helicopter blades /

Chattot, J. J.
Aeromechanics Laboratory.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.

January 1980

Oct. 1980."Aeromechanics Laboratory"--Cover.Includes bibliographical references.Mode of access: Inte...

Transonic pressure distributions on three rigid wings simulating paragliders with varied canopy curvature and leading edge sweep /

Fournier, Paul G.
Bell, B. Ann.
United States. National Aeronautics and Space Administration.

Cover title."January 1962."Aerodynamics, aircraft; Aerodynamics, missiles and space vehicles; Aircra...

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...

Calculation of the twist distribution of wings designed for cruise at transonic speeds /

Mann, Michael J.
Langley Research Center.

January 1974

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

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

Woodson, Shawn H.
DeJarnette, Fred R.
Langley Research Center.

January 1988

"October 1988"--Cover."Prepared for Langley Research Center under Cooperative Agreement NCC1-22."Inc...

A finite difference method for the solution of the transonic flow around harmonically oscillating wings /

Ehlers, F. Edward.
Langley Research Center.
Boeing Commercial Airplane Company.

January 1974

"Prepared by Boeing Commercial Aircraft Company ... for Langley Research Center."Cover title.Bibliog...

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. ...

Calculative techniques for transonic flows about certain classes of wing-body combinations /

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

January 1972

"Prepared by Nielsen Engineering & Research, Inc. ... for Ames Research Center."Cover title.Bibliogr...

The practical application of a finite difference method for analyzing transonic flow over oscillating airfoils and wings /

Ehlers, F. Edward, joint author.
Sebastian, James D., joint author.
Boeing Commercial Airplane Company.
Langley Research Center.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Office.

January 1978

Issued Feb. 1978.Prepared for Langley Research Center under Contact NAS 1-14204.Includes bibliograph...

Flow field analysis of aircraft configurations using a numerical solution to the three-dimensional unified supersonic/hypersonic small disturbance equations /

Gunness, R. C.
Dsylva, E.
Knight, C. J.
Langley Research Center.
Boeing Company.

January 1972

"February 1972."Cover title.Performed by the Boeing Company, Seattle, Wash., for Langley Research C...

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 ...

Computation of transonic potential flow about three-dimensional inlets, ducts, and bodies /

Reyhner, Theodore A.
Boeing Commercial Airplane Company.
Langley Research Center.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.

January 1982

Subject Category 02."March 1982"--Cover.Includes bibliographical references.Mode of access: Internet

Computation of the transonic perturbation flow fields around two- and three-dimensional oscillating wings

Weatherill, W. H.
Ehlers, F. E.
Sebastian, J. D.

December 1975

Analytical and empirical studies of a finite difference method for the solution of the transonic flo...

Calculation of the longitudinal aerodynamic characteristics of wing-flap configurations with externally blown flaps /

Mendenhall, M. R.
Langley Research Center.
Nielsen Engineering & Research.

"Prepared by Nielsen Engineering & Research, Inc. ... for Langley Research Center.""September 1976."...

Contribution to methods for calculating the flow about thin lifting wings at transonic speeds : Analytic expressions for the far field /

Klunker, E. B.
United States. National Aeronautics and Space Administration.
Langley Research Center.

January 1971

Prepared at Langley Research Center.N72-11289.Cover title.Includes bibliographical references (p. 15...

Calculation of three-dimensional unsteady transonic flows past helicopter blades /

Chattot, J. J.
Aeromechanics Laboratory.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.

January 1980

Oct. 1980."Aeromechanics Laboratory"--Cover.Includes bibliographical references.Mode of access: Inte...

Transonic pressure distributions on three rigid wings simulating paragliders with varied canopy curvature and leading edge sweep /

Fournier, Paul G.
Bell, B. Ann.
United States. National Aeronautics and Space Administration.

Cover title."January 1962."Aerodynamics, aircraft; Aerodynamics, missiles and space vehicles; Aircra...

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...

Calculation of the twist distribution of wings designed for cruise at transonic speeds /

Mann, Michael J.
Langley Research Center.

January 1974

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

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

Woodson, Shawn H.
DeJarnette, Fred R.
Langley Research Center.

January 1988

"October 1988"--Cover."Prepared for Langley Research Center under Cooperative Agreement NCC1-22."Inc...

Computation of the transonic perturbation flow fields around two- and three-dimensional oscillating wings /

Abstract

Extracted data

Computation of the transonic perturbation flow fields around two- and three-dimensional oscillating wings /

Abstract

Extracted data

Related items

Related items