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

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

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 Fortran program to calculate the flow field and performance of an axially symmetric deLaval nozzle /

Thompson, D.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Division.

January 1965

"January 1965"--Cover.Includes bibliographical references (p. 150).Mode of access: Internet

Assessment of an analytical procedure for predicting supersonic ejector nozzle performance /

Anderson, Bernhard H.
Lewis Research Center.

January 1974

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

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 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 ...

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

Cunningham, Herbert J.
Langley Research Center.

January 1974

Prepared at Langley Research Center.Cover title.Includes bibliographical references (p. [68]).Mode o...

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

The NCOREL computer program for 3D nonlinear supersonic potential flow computations /

Siclari, Michael J.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.
Langley Research Center.
Grumman Aerospace Corporation.

January 1983

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

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

Computer program for design analysis of radial-inflow turbines /

Glassman, Arthur J.
Lewis Research Center.

January 1976

Prepared at Lewis Research Center.Cover title.Includes bibliographical references (p. 58).Mode of ac...

Computer program for calculating full potential transonic, quasi-three-dimensional flow through a rotating turbomachinery blade row /

Farrell, Charles A.
Lewis Research Center.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.

January 1982

STAR category 02."June 1982"--Cover."Lewis Research Center."Includes bibliographical references.Mode...

Supersonic wind tunnel nozzles : a selected, annotated bibliography to aid in the development of quiet wind tunnel technology /

Wolf, Stephen W. D.
Ames Research Center. Fluid Dynamics Research Branch.

January 1990

Includes indexes.Sponsored by the Fluid Dynamics Research Branch, NASA Ames Research Center, under C...

Calculation of two-dimensional inlet flow fields in a supersonic free stream : program documentation and test cases /

Biringen, Sedat.
McMillan, Oden J.
Langley Research Center.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Office.

January 1980

"March 1980"--Cover.Includes bibliographical references.Mode of access: Internet

Calculation of axisymmetric supersonic flow past blunt bodies with sonic corners : including a program description and listing /

South, Jerry C. (Jerry Curtis), 1935-
Langley Research Center.
United States. National Aeronautics and Space Administration.

January 1968

Cover title."May 1968."Includes bibliographical references (p. 36-37).Mode of access: Internet

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

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 Fortran program to calculate the flow field and performance of an axially symmetric deLaval nozzle /

Thompson, D.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Division.

January 1965

"January 1965"--Cover.Includes bibliographical references (p. 150).Mode of access: Internet

Assessment of an analytical procedure for predicting supersonic ejector nozzle performance /

Anderson, Bernhard H.
Lewis Research Center.

January 1974

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

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 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 ...

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

Cunningham, Herbert J.
Langley Research Center.

January 1974

Prepared at Langley Research Center.Cover title.Includes bibliographical references (p. [68]).Mode o...

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

The NCOREL computer program for 3D nonlinear supersonic potential flow computations /

Siclari, Michael J.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.
Langley Research Center.
Grumman Aerospace Corporation.

January 1983

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

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

Computer program for design analysis of radial-inflow turbines /

Glassman, Arthur J.
Lewis Research Center.

January 1976

Prepared at Lewis Research Center.Cover title.Includes bibliographical references (p. 58).Mode of ac...

Computer program for calculating full potential transonic, quasi-three-dimensional flow through a rotating turbomachinery blade row /

Farrell, Charles A.
Lewis Research Center.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.

January 1982

STAR category 02."June 1982"--Cover."Lewis Research Center."Includes bibliographical references.Mode...

Supersonic wind tunnel nozzles : a selected, annotated bibliography to aid in the development of quiet wind tunnel technology /

Wolf, Stephen W. D.
Ames Research Center. Fluid Dynamics Research Branch.

January 1990

Includes indexes.Sponsored by the Fluid Dynamics Research Branch, NASA Ames Research Center, under C...

Calculation of two-dimensional inlet flow fields in a supersonic free stream : program documentation and test cases /

Biringen, Sedat.
McMillan, Oden J.
Langley Research Center.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Office.

January 1980

"March 1980"--Cover.Includes bibliographical references.Mode of access: Internet

Calculation of axisymmetric supersonic flow past blunt bodies with sonic corners : including a program description and listing /

South, Jerry C. (Jerry Curtis), 1935-
Langley Research Center.
United States. National Aeronautics and Space Administration.

January 1968

Cover title."May 1968."Includes bibliographical references (p. 36-37).Mode of access: Internet

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

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 Fortran program to calculate the flow field and performance of an axially symmetric deLaval nozzle /

Thompson, D.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Division.

January 1965

"January 1965"--Cover.Includes bibliographical references (p. 150).Mode of access: Internet

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

Abstract

Extracted data

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

Abstract

Extracted data

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