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 /

Low-speed wind-tunnel investigation of blowing boundary-layer control on leading- and trailing-edge flaps of a full-scale, low-aspect-ratio, 42° swept-wing airplane configuration /

Maki, Ralph L.
Giulianetti, Demo J.
Ames Research Center.

January 1959

"NASA TN D-16.""Ames Research Center, Moffett Field, Calif.""August 1959."Cover title.Includes bibli...

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...

Extension of leading-edge-suction analogy to wings with separated flow around the side edges at subsonic speeds /

Lamar, John E.
Langley Research Center.

January 1974

Prepared at Langley Research Center.Cover title.Includes bibliographical references (p. 24-25).Mode ...

Investigation of leading-edge flap performance on delta and double-delta wings at supersonic speeds /

Covell, Peter F.
Miller, David S.
Wood, Richard M.
Langley Research Center.

January 1987

Prepared at Langley Research Center."April 1987"--Cover.Includes bibliographical references (p. 6-7)...

A computer program to calculate the longitudinal aerodynamic characteristics of wing-flap configurations with extremely blown flaps /

Mendenhall, M. R.
Spangler, Selden B.
Goodwin, Frederick K.
Langley Research Center.
Nielsen Engineering & Research.

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

Natural laminar flow airfoil design considerations for winglets on low-speed airplanes /

Van Dam, C. P. (Cornelis P.), 1954-
Langley Research Center.
Vigyan Research Associates.

January 1984

"Prepared [at Vigyan Research Associates] for Langley Research Center under Contract NAS1-17797.""De...

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."...

Theoretical/numerical study of feasibility of use of winglets on low aspect ratio wings at subsonic and transonic Mach numbers to reduce drag /

Kuhlmann, John, 1948-
Cerney, Michael J.
Liaw, Paul.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Division.

January 1988

Prepared for Langley Research Center under Grant NAG1-625."August 1988"--Cover.Bibliography: p. 34-3...

A method for calculating aerodynamic loadings on thin wings at a Mach number of 1 /

Crigler, John L.
Langley Research Center.

Prepared at Langley Research Center."November 1959."Cover title.Includes bibliographical references ...

Numerical methods for the design and analysis of wings at supersonic speeds /

Carlson, Harry W.
Miller, David S.
Langley Research Center.

January 1974

Prepared at Langley Research Center.Cover title.Includes bibliographical references (p. 29-30).Mode ...

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 ...

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 longitudinal aerodynamic characteristics of upper-surface blown wing-flap configurations /

Mendenhall, Michael R.
Spangler, Selden B., joint author.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Office.

January 1978

Issued Aug. 1978.Prepared for Langley Research Center, by Nielsen Engineering & Research, Inc., unde...

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...

Simplified lifting-surface theory for flaps on wings of low and moderate aspect ratios /

Wick, Bradford H.
Ames Research Center.

January 1975

Prepared at Ames Research Center.Cover title.Includes bibliographical references (p. 7).Mode of acce...

Low-speed wind-tunnel investigation of blowing boundary-layer control on leading- and trailing-edge flaps of a full-scale, low-aspect-ratio, 42° swept-wing airplane configuration /

Maki, Ralph L.
Giulianetti, Demo J.
Ames Research Center.

January 1959

"NASA TN D-16.""Ames Research Center, Moffett Field, Calif.""August 1959."Cover title.Includes bibli...

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...

Extension of leading-edge-suction analogy to wings with separated flow around the side edges at subsonic speeds /

Lamar, John E.
Langley Research Center.

January 1974

Prepared at Langley Research Center.Cover title.Includes bibliographical references (p. 24-25).Mode ...

Investigation of leading-edge flap performance on delta and double-delta wings at supersonic speeds /

Covell, Peter F.
Miller, David S.
Wood, Richard M.
Langley Research Center.

January 1987

Prepared at Langley Research Center."April 1987"--Cover.Includes bibliographical references (p. 6-7)...

A computer program to calculate the longitudinal aerodynamic characteristics of wing-flap configurations with extremely blown flaps /

Mendenhall, M. R.
Spangler, Selden B.
Goodwin, Frederick K.
Langley Research Center.
Nielsen Engineering & Research.

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

Natural laminar flow airfoil design considerations for winglets on low-speed airplanes /

Van Dam, C. P. (Cornelis P.), 1954-
Langley Research Center.
Vigyan Research Associates.

January 1984

"Prepared [at Vigyan Research Associates] for Langley Research Center under Contract NAS1-17797.""De...

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."...

Theoretical/numerical study of feasibility of use of winglets on low aspect ratio wings at subsonic and transonic Mach numbers to reduce drag /

Kuhlmann, John, 1948-
Cerney, Michael J.
Liaw, Paul.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Division.

January 1988

Prepared for Langley Research Center under Grant NAG1-625."August 1988"--Cover.Bibliography: p. 34-3...

A method for calculating aerodynamic loadings on thin wings at a Mach number of 1 /

Crigler, John L.
Langley Research Center.

Prepared at Langley Research Center."November 1959."Cover title.Includes bibliographical references ...

Numerical methods for the design and analysis of wings at supersonic speeds /

Carlson, Harry W.
Miller, David S.
Langley Research Center.

January 1974

Prepared at Langley Research Center.Cover title.Includes bibliographical references (p. 29-30).Mode ...

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 ...

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 longitudinal aerodynamic characteristics of upper-surface blown wing-flap configurations /

Mendenhall, Michael R.
Spangler, Selden B., joint author.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Office.

January 1978

Issued Aug. 1978.Prepared for Langley Research Center, by Nielsen Engineering & Research, Inc., unde...

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...

Simplified lifting-surface theory for flaps on wings of low and moderate aspect ratios /

Wick, Bradford H.
Ames Research Center.

January 1975

Prepared at Ames Research Center.Cover title.Includes bibliographical references (p. 7).Mode of acce...

Low-speed wind-tunnel investigation of blowing boundary-layer control on leading- and trailing-edge flaps of a full-scale, low-aspect-ratio, 42° swept-wing airplane configuration /

Maki, Ralph L.
Giulianetti, Demo J.
Ames Research Center.

January 1959

"NASA TN D-16.""Ames Research Center, Moffett Field, Calif.""August 1959."Cover title.Includes bibli...

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...

Extension of leading-edge-suction analogy to wings with separated flow around the side edges at subsonic speeds /

Lamar, John E.
Langley Research Center.

January 1974

Prepared at Langley Research Center.Cover title.Includes bibliographical references (p. 24-25).Mode ...

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 /

Abstract

Extracted data

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 /

Abstract

Extracted data

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