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

Handbook of supersonic aerodynamics : Volume 2 / Johns Hopkins University, Applied Physics Laboratory.

Johns Hopkins University. Applied Physics Laboratory. author.
United States. Navy Department. Bureau of Ordnance. issuing body.
Johns Hopkins University. Applied Physics Laboratory. sponsor.

"Produced and edited by the Aerodynamics Handbook staff of the Johns Hopkins University Applied Phys...

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

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...

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

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 ...

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...

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

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 ...

Study of supersonic wings employing the attainable leading-edge thrust concept /

Middleton, W. D. (Wilbur D.), 1931-
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.
Boeing Commercial Airplane Company.
Langley Research Center.

January 1982

"Boeing Commercial Airplane Company.""November 1982"--Cover.Includes bibliographical references.Mode...

Aerodynamic characteristics of a supersonic fighter aircraft model at Mach 0.40 to 2.47 /

Capone, Francis J.
Arbiter, Dorothy.
Bare, E. Ann.
Langley Research Center.

January 1986

Prepared at Langley Research Center."April 1986"--Cover.Includes bibliographical references (p. 15-1...

Aerodynamic design guidelines and computer program for estimation of subsonic wind tunnel performance /

Eckert, William T.
Jope, Jean, jointh author.
Mort, Kenneth W.
North Carolina. Army Air Mobility Research and Development Laboratory.
Ames Research Center.
United States. National Aeronautics and Space Administration.

January 1977

Issued Oct. 1976.Prepared by North Carolina State University, Raleigh, N.C. for Lagley Research Cent...

Aerodynamic design and analysis system for supersonic aircraft. Part 2: User's manual

Coleman, R. G.
Lundry, J. L.
Middleton, W. D.

March 1975

An integrated system of computer programs for supersonic configurations is described. An explanation...

A computational system for aerodynamic design and analysis of supersonic aircraft. Part 2: User's manual

Lundry, J. L.
Middleton, W. D.
Coleman, R. G.

August 1976

An integrated system of computer programs was developed for the design and analysis of supersonic co...

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 ...

Supersonic aerodynamic characteristics of canard, tailless, and aft-tail configurations for two wing planforms /

Covell, Peter F.
Langley Research Center.

January 1985

Prepared at Langley Research Center."June 1985"--Cover.Includes bibliographical references (p. 66).M...

Handbook of supersonic aerodynamics : Volume 2 / Johns Hopkins University, Applied Physics Laboratory.

Johns Hopkins University. Applied Physics Laboratory. author.
United States. Navy Department. Bureau of Ordnance. issuing body.
Johns Hopkins University. Applied Physics Laboratory. sponsor.

"Produced and edited by the Aerodynamics Handbook staff of the Johns Hopkins University Applied Phys...

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

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...

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

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 ...

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...

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

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 ...

Study of supersonic wings employing the attainable leading-edge thrust concept /

Middleton, W. D. (Wilbur D.), 1931-
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.
Boeing Commercial Airplane Company.
Langley Research Center.

January 1982

"Boeing Commercial Airplane Company.""November 1982"--Cover.Includes bibliographical references.Mode...

Aerodynamic characteristics of a supersonic fighter aircraft model at Mach 0.40 to 2.47 /

Capone, Francis J.
Arbiter, Dorothy.
Bare, E. Ann.
Langley Research Center.

January 1986

Prepared at Langley Research Center."April 1986"--Cover.Includes bibliographical references (p. 15-1...

Aerodynamic design guidelines and computer program for estimation of subsonic wind tunnel performance /

Eckert, William T.
Jope, Jean, jointh author.
Mort, Kenneth W.
North Carolina. Army Air Mobility Research and Development Laboratory.
Ames Research Center.
United States. National Aeronautics and Space Administration.

January 1977

Issued Oct. 1976.Prepared by North Carolina State University, Raleigh, N.C. for Lagley Research Cent...

Aerodynamic design and analysis system for supersonic aircraft. Part 2: User's manual

Coleman, R. G.
Lundry, J. L.
Middleton, W. D.

March 1975

An integrated system of computer programs for supersonic configurations is described. An explanation...

A computational system for aerodynamic design and analysis of supersonic aircraft. Part 2: User's manual

Lundry, J. L.
Middleton, W. D.
Coleman, R. G.

August 1976

An integrated system of computer programs was developed for the design and analysis of supersonic co...

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 ...

Supersonic aerodynamic characteristics of canard, tailless, and aft-tail configurations for two wing planforms /

Covell, Peter F.
Langley Research Center.

January 1985

Prepared at Langley Research Center."June 1985"--Cover.Includes bibliographical references (p. 66).M...

Handbook of supersonic aerodynamics : Volume 2 / Johns Hopkins University, Applied Physics Laboratory.

Johns Hopkins University. Applied Physics Laboratory. author.
United States. Navy Department. Bureau of Ordnance. issuing body.
Johns Hopkins University. Applied Physics Laboratory. sponsor.

"Produced and edited by the Aerodynamics Handbook staff of the Johns Hopkins University Applied Phys...

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

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...

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

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

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