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

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

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 ...

Aerodynamic characteristics of a 1/6-scale model of the rotor systems research aircraft with the rotors removed /

Mineck, Raymond E.
Hassell, James L., joint author.
Freeman, Carl E., joint author.
Langley Research Center.
United States. National Aeronautics and Space Administration.

January 1976

Cover title.Includes bibliographical references (p. 23).Mode of access: Internet

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 computational system for aerodynamic design and analysis of supersonic aircraft : part 2, user's manual /

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

January 1976

Issued Aug. 1976.Prepared by Boeing Commercial Airplane Company under contract no. NAS1-13732.Includ...

A System for aerodynamic design and analysis of supersonic aircraft.

Coleman, R. G. (Ronald Gene), 1939-
Lundry, J. L.
Middleton, W. D. (Wilbur D.), 1931-
Langley Research Center.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.

January 1980

Dec. 1980.Prepared for Langley Research Center, under contract NAS1-15534.Includes bibliographical r...

Aerodynamic design and analysis system for supersonic aircraft /

Middleton, W. D. (Wilbur D.), 1931-
Coleman, R. G. (Ronald Gene), 1939-
Lundry, J. L.
Langley Research Center.
Boeing Commercial Airplane Company.

"Prepared by Boeing Commercial Airplane Company ... for Langley Research Center.""March 1975."Cover ...

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 ...

Low-speed investigation of the aerodynamic characteristics of a variable-sweep supersonic transport configuration having a blended wing and body /

Sleeman, William C.
Robins, A. Warner.
Langley Research Center.

Cover title.Includes bibliographical references (p. 18).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

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 ...

Numerical solutions for supersonic flow of an ideal gas around blunt two-dimensional bodies /

Fuller, Franklyn B.
United States. National Aeronautics and Space Administration.

Cover title."July 1961."Aerodynamics, aircraft; Aerodynamics, missiles and space vehicles; Fluid mec...

Theoretical and experimental investigation of supersonic aerodynamic characteristics of a twin-fuselage concept /

Wood, Richard M.
Brentner, Kenneth S.
Miller, D. S. (David S.)
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.

January 1983

Distributed to depository libraries in microfiche."August 1983"--Cover.Subject category 02.Includes ...

A study of methods which predict supersonic flow fields from body geometry, distance, and Mach number /

Mack, Robert J.
Langley Research Center.

January 1973

Prepared at Langley Research Center.Cover title.Includes bibliographical references (p. 13-14).Mode ...

Development of a computer code for calculating the steady super/hypersonic inviscid flow around real configurations : volume I-computational technique /

Marconi, Frank.
Yaeger, Larry, joint author.
Salas, Manuel, joint author.
United States. National Aeronautics and Space Administration.
Grumman Aerospace Corporation.

January 1976

Cover title.Includes bibliographical references (p. 87-88).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

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 ...

Aerodynamic characteristics of a 1/6-scale model of the rotor systems research aircraft with the rotors removed /

Mineck, Raymond E.
Hassell, James L., joint author.
Freeman, Carl E., joint author.
Langley Research Center.
United States. National Aeronautics and Space Administration.

January 1976

Cover title.Includes bibliographical references (p. 23).Mode of access: Internet

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 computational system for aerodynamic design and analysis of supersonic aircraft : part 2, user's manual /

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

January 1976

Issued Aug. 1976.Prepared by Boeing Commercial Airplane Company under contract no. NAS1-13732.Includ...

A System for aerodynamic design and analysis of supersonic aircraft.

Coleman, R. G. (Ronald Gene), 1939-
Lundry, J. L.
Middleton, W. D. (Wilbur D.), 1931-
Langley Research Center.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.

January 1980

Dec. 1980.Prepared for Langley Research Center, under contract NAS1-15534.Includes bibliographical r...

Aerodynamic design and analysis system for supersonic aircraft /

Middleton, W. D. (Wilbur D.), 1931-
Coleman, R. G. (Ronald Gene), 1939-
Lundry, J. L.
Langley Research Center.
Boeing Commercial Airplane Company.

"Prepared by Boeing Commercial Airplane Company ... for Langley Research Center.""March 1975."Cover ...

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 ...

Low-speed investigation of the aerodynamic characteristics of a variable-sweep supersonic transport configuration having a blended wing and body /

Sleeman, William C.
Robins, A. Warner.
Langley Research Center.

Cover title.Includes bibliographical references (p. 18).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

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 ...

Numerical solutions for supersonic flow of an ideal gas around blunt two-dimensional bodies /

Fuller, Franklyn B.
United States. National Aeronautics and Space Administration.

Cover title."July 1961."Aerodynamics, aircraft; Aerodynamics, missiles and space vehicles; Fluid mec...

Theoretical and experimental investigation of supersonic aerodynamic characteristics of a twin-fuselage concept /

Wood, Richard M.
Brentner, Kenneth S.
Miller, D. S. (David S.)
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.

January 1983

Distributed to depository libraries in microfiche."August 1983"--Cover.Subject category 02.Includes ...

A study of methods which predict supersonic flow fields from body geometry, distance, and Mach number /

Mack, Robert J.
Langley Research Center.

January 1973

Prepared at Langley Research Center.Cover title.Includes bibliographical references (p. 13-14).Mode ...

Development of a computer code for calculating the steady super/hypersonic inviscid flow around real configurations : volume I-computational technique /

Marconi, Frank.
Yaeger, Larry, joint author.
Salas, Manuel, joint author.
United States. National Aeronautics and Space Administration.
Grumman Aerospace Corporation.

January 1976

Cover title.Includes bibliographical references (p. 87-88).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

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 ...

Aerodynamic characteristics of a 1/6-scale model of the rotor systems research aircraft with the rotors removed /

Mineck, Raymond E.
Hassell, James L., joint author.
Freeman, Carl E., joint author.
Langley Research Center.
United States. National Aeronautics and Space Administration.

January 1976

Cover title.Includes bibliographical references (p. 23).Mode of access: Internet

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

Abstract

Extracted data

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

Abstract

Extracted data

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