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

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 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 ...

Longitudinal aerodynamic characteristics of a vectored-engine-over-wing configuration at subsonic speeds /

Leavitt, Laurence D.
Langley Research Center.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.

January 1979

"October 1979"--Cover."Langley Research Center."Includes bibliographical references.Mode of access: ...

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...

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."...

Calculation of the longitudinal aerodynamic characteristics of STOL aircraft with externally-blown jet-augmented flaps /

Dillenius, Marnix F. E., 1938-
Spangler, Selden B.
Mendenhall, M. R.
Ames Research Center.
Nielsen Engineering & Research.

January 1974

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

Longitudinal aerodynamic characteristics of an externally blown flap powered-lift model with several propulsive system simulators /

Hoad, Danny R.
Langley Research Center.

January 1974

Prepared at Langley Research Center.Cover title.Includes bibliographical references (p. 15).Mode of ...

Computer programs for calculating the static longitudinal aerodynamic characteristics of wing-body-tail configurations /

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

January 1975

"Prepared by Nielsen Engineering & Research ... for Ames Research Center."Cover title.Includes bibli...

Wind-tunnel investigation of aerodynamic loads on a large-scale externally blown flap model and comparison with theory /

Perry, Boyd.
Greene, George C.
Langley Research Center.

January 1975

Prepared at Langley Research Center.Cover title.Includes bibliographical references (p. 14-15).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 /

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

January 1987

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

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...

Wind-tunnel investigation of effects of variations in Reynolds number and leading-edge treatment on the aerodynamic characteristics of an externally blown jet-flap configuration /

Parlett, Lysle P.
Megrail, James L.
Smith, Charles Christian, 1921-
Langley Research Center.

January 1973

Research prepared at Langley Research Center.Cover title.Bibliography: p. 8.Mode of access: Internet

Effect of wing aspect ratio and flap span on aerodynamic characteristics of an externally blown jet-flap STOL model /

Smith, Charles Christian, 1921-
Langley Research Center.

January 1973

Research prepared at Langley Research Center.Cover title.Bibliography: p. 9.Mode of access: Internet

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)...

Longitudinal aerodynamic characteristics at transonic speeds of two V/STOL airplane configurations with skewed and variable-sweep wings /

Luoma, Arvo A.
Langley Research Center.

January 1961

"April 1961."Cover title.Includes bibliographical references (p. 14-15).Mode of access: Internet

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 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 ...

Longitudinal aerodynamic characteristics of a vectored-engine-over-wing configuration at subsonic speeds /

Leavitt, Laurence D.
Langley Research Center.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.

January 1979

"October 1979"--Cover."Langley Research Center."Includes bibliographical references.Mode of access: ...

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...

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."...

Calculation of the longitudinal aerodynamic characteristics of STOL aircraft with externally-blown jet-augmented flaps /

Dillenius, Marnix F. E., 1938-
Spangler, Selden B.
Mendenhall, M. R.
Ames Research Center.
Nielsen Engineering & Research.

January 1974

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

Longitudinal aerodynamic characteristics of an externally blown flap powered-lift model with several propulsive system simulators /

Hoad, Danny R.
Langley Research Center.

January 1974

Prepared at Langley Research Center.Cover title.Includes bibliographical references (p. 15).Mode of ...

Computer programs for calculating the static longitudinal aerodynamic characteristics of wing-body-tail configurations /

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

January 1975

"Prepared by Nielsen Engineering & Research ... for Ames Research Center."Cover title.Includes bibli...

Wind-tunnel investigation of aerodynamic loads on a large-scale externally blown flap model and comparison with theory /

Perry, Boyd.
Greene, George C.
Langley Research Center.

January 1975

Prepared at Langley Research Center.Cover title.Includes bibliographical references (p. 14-15).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 /

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

January 1987

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

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...

Wind-tunnel investigation of effects of variations in Reynolds number and leading-edge treatment on the aerodynamic characteristics of an externally blown jet-flap configuration /

Parlett, Lysle P.
Megrail, James L.
Smith, Charles Christian, 1921-
Langley Research Center.

January 1973

Research prepared at Langley Research Center.Cover title.Bibliography: p. 8.Mode of access: Internet

Effect of wing aspect ratio and flap span on aerodynamic characteristics of an externally blown jet-flap STOL model /

Smith, Charles Christian, 1921-
Langley Research Center.

January 1973

Research prepared at Langley Research Center.Cover title.Bibliography: p. 9.Mode of access: Internet

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)...

Longitudinal aerodynamic characteristics at transonic speeds of two V/STOL airplane configurations with skewed and variable-sweep wings /

Luoma, Arvo A.
Langley Research Center.

January 1961

"April 1961."Cover title.Includes bibliographical references (p. 14-15).Mode of access: Internet

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 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 ...

Longitudinal aerodynamic characteristics of a vectored-engine-over-wing configuration at subsonic speeds /

Leavitt, Laurence D.
Langley Research Center.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.

January 1979

"October 1979"--Cover."Langley Research Center."Includes bibliographical references.Mode of access: ...

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

Abstract

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

Abstract

Extracted data

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