Use of CYBER 203 and CYBER 205 computers for three-dimensional transonic flow calculations /

A linear aerodynamic analysis for unsteady transonic cascades /

Verdon, Joseph M.
Caspar, Joseph R.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.
Lewis Research Center.

STAR category 02.Distributed to depository libraries in microfiche."September 1984"--Cover.Includes ...

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...

Development of a three-dimensional supersonic inlet flow analysis /

Buggeln, R. C.
Lewis Research Center.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Office.

January 1980

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

Transonic flow analysis for rotors.

Chang, I-Chung.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Division.

January 1990

"June 1990."Cover title.Distributed to depository libraries in microfiche.Includes bibliographical r...

Computation of transonic potential flow about three-dimensional inlets, ducts, and bodies /

Reyhner, Theodore A.
Boeing Commercial Airplane Company.
Langley Research Center.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.

January 1982

Subject Category 02."March 1982"--Cover.Includes bibliographical references.Mode of access: Internet

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...

A Numerical simulation of three-dimensional flow in an adaptive wall wind tunnel /

Mendoza, J. P.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.

"August 1984."Distributed to depository libraries in microfiche.Includes bibliographical references....

Numerical calculations of two-dimensional, unsteady transonic flows with circulation /

Beam, Richard M.
Warming, Robert F. (Robert Fulton)
Ames Research Center.

January 1974

Prepared at Ames Research Center.Cover title.Includes bibliographical references (p. 21-22).Mode of ...

Aerodynamic design for improved maneuverability by use of three-dimensional transonic theory /

Mann, Michael J.
Ferris, James C.
Campbell, Richard L. (Richard Lawson), 1952-
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.

January 1984

Subject category 02."February 1984"--Cover.Distributed to depository libraries in microfiche.Include...

Calculation of three-dimensional unsteady transonic flows past helicopter blades /

Chattot, J. J.
Aeromechanics Laboratory.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.

January 1980

Oct. 1980."Aeromechanics Laboratory"--Cover.Includes bibliographical references.Mode of access: Inte...

Calculations of inviscid flow over shuttle-like vehicles at high angles of attack and comparisons with experimental data /

Weilmuenster, K. James.
Hamilton, H. Harris.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.

January 1983

Distributed to depository libraries in microfiche."May 1983"--Cover.Includes bibliographical referen...

FORTRAN program for quasi-three-dimensional calculation of surface velocities and choking flow for turbomachine blade rows /

Katsanis, Theodore.

"April 1971."Cover title.Includes bibliographical references (p. 30).Mode of access: Internet

A supersonic three-dimensional code for flow over blunt bodies : program documentation and test cases /

Chaussee, D. S.
McMillan, Oden J.
Langley Research Center.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Office.

January 1980

"February 1980"--Cover.Includes Bibliographical reference.Mode of access: Internet

Development of a locally mass flux conservative computer code for calculating 3-D viscous flow in turbomachines /

Walitt, Leonard.
Lewis Research Center.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.

January 1982

STAR Category 02."April 1982"--Cover.Includes bibliographical references.Mode of access: Internet

Numerical computation of transonic flows by finite-element and finite-diffence methods /

United States. National Aeronautics and Space Administration. Scientific and Technical Information Office.
Hafez, M. M.
Langley Research Center.
Flow Research, inc.

January 1978

Dec. 1978.Contract NAS1-14246.Includes bibliographical references.Mode of access: Internet

A linear aerodynamic analysis for unsteady transonic cascades /

Verdon, Joseph M.
Caspar, Joseph R.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.
Lewis Research Center.

STAR category 02.Distributed to depository libraries in microfiche."September 1984"--Cover.Includes ...

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...

Development of a three-dimensional supersonic inlet flow analysis /

Buggeln, R. C.
Lewis Research Center.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Office.

January 1980

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

Transonic flow analysis for rotors.

Chang, I-Chung.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Division.

January 1990

"June 1990."Cover title.Distributed to depository libraries in microfiche.Includes bibliographical r...

Computation of transonic potential flow about three-dimensional inlets, ducts, and bodies /

Reyhner, Theodore A.
Boeing Commercial Airplane Company.
Langley Research Center.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.

January 1982

Subject Category 02."March 1982"--Cover.Includes bibliographical references.Mode of access: Internet

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...

A Numerical simulation of three-dimensional flow in an adaptive wall wind tunnel /

Mendoza, J. P.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.

"August 1984."Distributed to depository libraries in microfiche.Includes bibliographical references....

Numerical calculations of two-dimensional, unsteady transonic flows with circulation /

Beam, Richard M.
Warming, Robert F. (Robert Fulton)
Ames Research Center.

January 1974

Prepared at Ames Research Center.Cover title.Includes bibliographical references (p. 21-22).Mode of ...

Aerodynamic design for improved maneuverability by use of three-dimensional transonic theory /

Mann, Michael J.
Ferris, James C.
Campbell, Richard L. (Richard Lawson), 1952-
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.

January 1984

Subject category 02."February 1984"--Cover.Distributed to depository libraries in microfiche.Include...

Calculation of three-dimensional unsteady transonic flows past helicopter blades /

Chattot, J. J.
Aeromechanics Laboratory.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.

January 1980

Oct. 1980."Aeromechanics Laboratory"--Cover.Includes bibliographical references.Mode of access: Inte...

Calculations of inviscid flow over shuttle-like vehicles at high angles of attack and comparisons with experimental data /

Weilmuenster, K. James.
Hamilton, H. Harris.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.

January 1983

Distributed to depository libraries in microfiche."May 1983"--Cover.Includes bibliographical referen...

FORTRAN program for quasi-three-dimensional calculation of surface velocities and choking flow for turbomachine blade rows /

Katsanis, Theodore.

"April 1971."Cover title.Includes bibliographical references (p. 30).Mode of access: Internet

A supersonic three-dimensional code for flow over blunt bodies : program documentation and test cases /

Chaussee, D. S.
McMillan, Oden J.
Langley Research Center.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Office.

January 1980

"February 1980"--Cover.Includes Bibliographical reference.Mode of access: Internet

Development of a locally mass flux conservative computer code for calculating 3-D viscous flow in turbomachines /

Walitt, Leonard.
Lewis Research Center.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.

January 1982

STAR Category 02."April 1982"--Cover.Includes bibliographical references.Mode of access: Internet

Numerical computation of transonic flows by finite-element and finite-diffence methods /

United States. National Aeronautics and Space Administration. Scientific and Technical Information Office.
Hafez, M. M.
Langley Research Center.
Flow Research, inc.

January 1978

Dec. 1978.Contract NAS1-14246.Includes bibliographical references.Mode of access: Internet

A linear aerodynamic analysis for unsteady transonic cascades /

Verdon, Joseph M.
Caspar, Joseph R.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.
Lewis Research Center.

STAR category 02.Distributed to depository libraries in microfiche."September 1984"--Cover.Includes ...

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...

Development of a three-dimensional supersonic inlet flow analysis /

Buggeln, R. C.
Lewis Research Center.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Office.

January 1980

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

Use of CYBER 203 and CYBER 205 computers for three-dimensional transonic flow calculations /

Abstract

Extracted data

Use of CYBER 203 and CYBER 205 computers for three-dimensional transonic flow calculations /

Abstract

Extracted data

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