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

Fortran program for calculating the static longitudinal aerodynamic characteristics of wing-body-tail configurations including vortex lift from sharp edges

Dutt, HNV

August 1986

This project document is a User's manual for computer13; program for calculating the longitudinal ae...

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 ...

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."...

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."...

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...

Effect of symmetrical vortex shedding on the longitudinal aerodynamic characteristics of wing-body-tail combinations /

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

January 1975

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

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

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...

Calculative techniques for transonic flows about certain classes of wing-body combinations /

Stahara, Stephen S.
Spreiter, John R.
Ames Research Center.
Nielsen Engineering & Research.

January 1972

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

On the formulation of the aerodynamic characteristics in aircraft dynamics /

Tobak, Murray.
Schiff, Lewis B.
Ames Research Center.

January 1976

Prepared at Ames Research Center."Corrected copy."Cover title.Includes bibliographical references (p...

Static longitudinal and lateral aerodynamic characteristics at a Mach number of 2.20 of a variable-wing-sweep STOL configuration /

Foster, Gerald V.
Morris, Odell A.
Langley Research Center.
United States. National Aeronautics and Space Administration.

January 1960

"October 1960."Cover title.Includes bibliographical references (p. 7-8).Mode of access: Internet

Static longitudinal aerodynamic characteristics at a Mach number of 10.03 of low-aspect-ratio wing-body configurations suitable for reentry /

Putnam, Lawrence E. (Lawrence Elwood)
Brooks, Cuyler W.
Langley Research Center.

January 1962

"December 1962."Cover title.Includes bibliographical references (p. 9).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

Transonic investigation of the static longitudinal aerodynamic characteristics of low-aspect-ratio wing-body configurations at angles of attack from 0⁰ to 90⁰ /

Trescot, Charles D.
Brooks, Cuyler W.
Putman, Lawrence E.
United States. National Aeronautics and Space Administration.

Cover title."June 1963."Includes bibliographical references.Mode of access: Internet

Fortran program for calculating the static longitudinal aerodynamic characteristics of wing-body-tail configurations including vortex lift from sharp edges

Dutt, HNV

August 1986

This project document is a User's manual for computer13; program for calculating the longitudinal ae...

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 ...

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."...

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."...

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...

Effect of symmetrical vortex shedding on the longitudinal aerodynamic characteristics of wing-body-tail combinations /

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

January 1975

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

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

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...

Calculative techniques for transonic flows about certain classes of wing-body combinations /

Stahara, Stephen S.
Spreiter, John R.
Ames Research Center.
Nielsen Engineering & Research.

January 1972

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

On the formulation of the aerodynamic characteristics in aircraft dynamics /

Tobak, Murray.
Schiff, Lewis B.
Ames Research Center.

January 1976

Prepared at Ames Research Center."Corrected copy."Cover title.Includes bibliographical references (p...

Static longitudinal and lateral aerodynamic characteristics at a Mach number of 2.20 of a variable-wing-sweep STOL configuration /

Foster, Gerald V.
Morris, Odell A.
Langley Research Center.
United States. National Aeronautics and Space Administration.

January 1960

"October 1960."Cover title.Includes bibliographical references (p. 7-8).Mode of access: Internet

Static longitudinal aerodynamic characteristics at a Mach number of 10.03 of low-aspect-ratio wing-body configurations suitable for reentry /

Putnam, Lawrence E. (Lawrence Elwood)
Brooks, Cuyler W.
Langley Research Center.

January 1962

"December 1962."Cover title.Includes bibliographical references (p. 9).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

Transonic investigation of the static longitudinal aerodynamic characteristics of low-aspect-ratio wing-body configurations at angles of attack from 0⁰ to 90⁰ /

Trescot, Charles D.
Brooks, Cuyler W.
Putman, Lawrence E.
United States. National Aeronautics and Space Administration.

Cover title."June 1963."Includes bibliographical references.Mode of access: Internet

Fortran program for calculating the static longitudinal aerodynamic characteristics of wing-body-tail configurations including vortex lift from sharp edges

Dutt, HNV

August 1986

This project document is a User's manual for computer13; program for calculating the longitudinal ae...

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 ...

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 ...

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

Abstract

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

Abstract

Extracted data

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