Computer program for supersonic kernel-function flutter analysis of thin lifting surfaces /

Wind-tunnel investigation of an upper surface blown jet-flap powered-lift configuration /

Phelps, Arthur E.
Smith, Charles Christian, 1921-
Langley Research Center.

January 1973

Prepared at Langley Research Center.Cover title.Includes bibliographical references (p. 11).Mode of ...

Investigation of the static lift capability of a low-aspect-ratio wing operating in a powered ground-effect mode /

Huffman, Jarrett K.
Jackson, Charlie M.
Langley Research Center.

January 1974

Prepared at Langley Research Center.Cover title.Includes bibliographical references (p. 3).Mode of a...

A computer program for the design and analysis of low-speed airfoils /

Eppler, Richard A.
Somers, Dan M.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.

January 1980

"August 1980"--Cover.Includes bibliographical reference (p. 126).Mode of access: Internet

Flutter analysis of swept-wing subsonic aircraft with parameter studies of composite wings /

Housner, Jerrold M.
Stein, Manuel.
Langley Research Center.

January 1974

Prepared at Langley Research Center.Cover title.Includes bibliographical references (p. 93).Mode of ...

Supersonic flutter of panels loaded with inplane shear /

Sawyer, James Wayne, 1941-
Langely Research Center.

January 1975

Prepared at Langley Research Center.Cover title.Includes bibliographical references (p. 16).Mode of ...

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 ...

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."...

A computational system for aerodynamic design and analysis of supersonic aircraft : part 3-computer program description /

Middleton, W. D.
Coleman, Robert Griffin, 1923- joint author.
Lundry, J. L., joint author.
United States. National Aeronautics and Space Administration.
Boeing Company.
Langley Research Center.

January 1976

Cover title.Includes bibliographical references (p. 99).Mode of access: Internet

A computer program for wing subsonic aerodynamic performance estimates including attainable thrust and vortex lift effects /

Carlson, Harry W.
Walkley, Kenneth B.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.
Langley Research Center.

January 1982

Subject Category 01."March 1982"--Cover.Includes bibliographical references.Mode of access: Internet

Study of flutter related computational procedures for minimum weight structural sizing of advanced aircraft /

O'Connell, Robert F.
Radovcich, N. A., joint author.
Hassig, H. J., joint author.
Lockheed-California Company.
United States. National Aeronautics and Space Administration.

January 1976

Cover title.Includes bibliographical references (p. 115-117).Mode of access: Internet

Flutter analysis and testing of pairs of aerodynamically interfering delta wings /

Chipman, Richard R.
Rauch, Frank J.
Langley Research Center.
Grumman Aerospace Corporation.

January 1973

"Prepared by Grumann Aerospace Corporation ... for Langley Research Center."Cover title.Bibliography...

Computer program for calculating the flow field of supersonic ejector nozzles /

Anderson, Bernhard H.
Lewis Research Center.

January 1974

Prepared at Lewis Research Center.Cover title.Includes bibliographical references (p. 83).Mode of ac...

Automated procedure for design of wing structures to satisfy strength and flutter requirements /

Haftka, Raphael T.
Langley Research Center.

January 1973

Prepared at Langley Research Center.Cover title.Bibliography: p. 22-24.Mode of access: Internet

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 ...

A computational system for aerodynamic design and analysis of supersonic aircraft : part 1-general description and theoretical development /

Middleton, W. D.
Lundry, J. L., joint author.
United States. National Aeronautics and Space Administration.
Boeing Company.
Langley Research Center.

January 1976

Cover title.Includes bibliographical references (p. 79-80).Mode of access: Internet

Wind-tunnel investigation of an upper surface blown jet-flap powered-lift configuration /

Phelps, Arthur E.
Smith, Charles Christian, 1921-
Langley Research Center.

January 1973

Prepared at Langley Research Center.Cover title.Includes bibliographical references (p. 11).Mode of ...

Investigation of the static lift capability of a low-aspect-ratio wing operating in a powered ground-effect mode /

Huffman, Jarrett K.
Jackson, Charlie M.
Langley Research Center.

January 1974

Prepared at Langley Research Center.Cover title.Includes bibliographical references (p. 3).Mode of a...

A computer program for the design and analysis of low-speed airfoils /

Eppler, Richard A.
Somers, Dan M.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.

January 1980

"August 1980"--Cover.Includes bibliographical reference (p. 126).Mode of access: Internet

Flutter analysis of swept-wing subsonic aircraft with parameter studies of composite wings /

Housner, Jerrold M.
Stein, Manuel.
Langley Research Center.

January 1974

Prepared at Langley Research Center.Cover title.Includes bibliographical references (p. 93).Mode of ...

Supersonic flutter of panels loaded with inplane shear /

Sawyer, James Wayne, 1941-
Langely Research Center.

January 1975

Prepared at Langley Research Center.Cover title.Includes bibliographical references (p. 16).Mode of ...

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 ...

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."...

A computational system for aerodynamic design and analysis of supersonic aircraft : part 3-computer program description /

Middleton, W. D.
Coleman, Robert Griffin, 1923- joint author.
Lundry, J. L., joint author.
United States. National Aeronautics and Space Administration.
Boeing Company.
Langley Research Center.

January 1976

Cover title.Includes bibliographical references (p. 99).Mode of access: Internet

A computer program for wing subsonic aerodynamic performance estimates including attainable thrust and vortex lift effects /

Carlson, Harry W.
Walkley, Kenneth B.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.
Langley Research Center.

January 1982

Subject Category 01."March 1982"--Cover.Includes bibliographical references.Mode of access: Internet

Study of flutter related computational procedures for minimum weight structural sizing of advanced aircraft /

O'Connell, Robert F.
Radovcich, N. A., joint author.
Hassig, H. J., joint author.
Lockheed-California Company.
United States. National Aeronautics and Space Administration.

January 1976

Cover title.Includes bibliographical references (p. 115-117).Mode of access: Internet

Flutter analysis and testing of pairs of aerodynamically interfering delta wings /

Chipman, Richard R.
Rauch, Frank J.
Langley Research Center.
Grumman Aerospace Corporation.

January 1973

"Prepared by Grumann Aerospace Corporation ... for Langley Research Center."Cover title.Bibliography...

Computer program for calculating the flow field of supersonic ejector nozzles /

Anderson, Bernhard H.
Lewis Research Center.

January 1974

Prepared at Lewis Research Center.Cover title.Includes bibliographical references (p. 83).Mode of ac...

Automated procedure for design of wing structures to satisfy strength and flutter requirements /

Haftka, Raphael T.
Langley Research Center.

January 1973

Prepared at Langley Research Center.Cover title.Bibliography: p. 22-24.Mode of access: Internet

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 ...

A computational system for aerodynamic design and analysis of supersonic aircraft : part 1-general description and theoretical development /

Middleton, W. D.
Lundry, J. L., joint author.
United States. National Aeronautics and Space Administration.
Boeing Company.
Langley Research Center.

January 1976

Cover title.Includes bibliographical references (p. 79-80).Mode of access: Internet

Wind-tunnel investigation of an upper surface blown jet-flap powered-lift configuration /

Phelps, Arthur E.
Smith, Charles Christian, 1921-
Langley Research Center.

January 1973

Prepared at Langley Research Center.Cover title.Includes bibliographical references (p. 11).Mode of ...

Investigation of the static lift capability of a low-aspect-ratio wing operating in a powered ground-effect mode /

Huffman, Jarrett K.
Jackson, Charlie M.
Langley Research Center.

January 1974

Prepared at Langley Research Center.Cover title.Includes bibliographical references (p. 3).Mode of a...

A computer program for the design and analysis of low-speed airfoils /

Eppler, Richard A.
Somers, Dan M.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.

January 1980

"August 1980"--Cover.Includes bibliographical reference (p. 126).Mode of access: Internet

Computer program for supersonic kernel-function flutter analysis of thin lifting surfaces /

Abstract

Extracted data

Computer program for supersonic kernel-function flutter analysis of thin lifting surfaces /

Abstract

Extracted data

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