The development of a three-dimensional partially elliptic flow computer program for combustor research /

Computation of three-dimensional nozzle-exhaust flow fields with the GIM code /

Spradley, L. W.
Pearson, M. L. (Marcus Lowell), 1941- joint author.
Anderson, P. G., joint author.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Office.

Issued Augt. 1978.Prepared for Langley Research Center, by Lockheed Missiles and Space Co., Inc., un...

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

Anderson, Bernhard H.
Lewis Research Center.

January 1974

Prepared at Lewis Research Center.Cover title.Includes bibliographical references (p. 83).Mode of ac...

A simplified computer program for the prediction of the linear stability behavior of liquid propellant combustors /

Mitchell, C. E.
Eckert, K.
Lewis Research Center.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.

January 1979

STAR category no. 20."August 1979"--Cover.Includes bibliographical references.Mode of access: Intern...

The AEDC three-dimensional, potential flow computer program.

Todd, Donald C., author.
ARO, Inc. sponsor.
United States. Air Force. Arnold Air Force Base. sponsor.
United States. Air Force. Systems Command. Arnold Engineering Development Center. issuing body.

"Program Element 65807.""Final Report for Period November 1971--November 1974.""February 1976."Inclu...

Combustion of hydrogen injected into a supersonic airstream (the ship computer program) /

Markatos, N. C.
Tatchell, D. G., joint author.
Spalding, D. B. (Dudley Brian), 1923- joint author.
Fluid Mechanics and Thermal Systems.
United States. National Aeronautics and Space Administration.

January 1977

Issued April 1977.Prepared by Fluid Mechanics and Thermal Systems, Inc. for Langley Research Center ...

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...

An improved supersonic, three-dimensional, external, inviscid flow field code /

Marconi, Frank.
Koch, Frank, 1931- joint author.
Grumman Aerospace Corporation.
Langley Research Center.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Office.

January 1979

March 1979.Prepared for Langley Research Center under contract NAS1-14162.Includes bibliographical r...

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

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

An approximate method for calculating three-dimensional inviscid hypersonic flow fields /

Riley, Christopher J. (Christopher Joseph), 1964-
DeJarnette, Fred R.
Langley Research Center.

January 1990

Prepared at Langley Research Center.Bibliography: p. 12.Mode of access: Internet

Investigations of three dimensional flow characteristics in a three bladed rocket pump inducer /

Poncet, A.
Lakshminarayana, B.
Lewis Research Center.
Pennsylvania State University.

January 1973

"Prepared by Pennsylvania State University ... for Lewis Research Center."Cover title.Bibliography: ...

Development of a three-dimensional turbulent duct flow analysis /

United States. National Aeronautics and Space Administration. Scientific and Technical Information Office.
Eiseman, P. R.
Lewis Research Center.
United Technologies Research Center.

January 1978

Nov. 1978.Contract NAS3-19856.Includes bibliographical references.Mode of access: Internet

Calculating three-dimensional flows around structures and over rough terrain /

Hirt, C. W.
Cook, J. L.
Los Alamos Scientific Laboratory.
U.S. Atomic Energy Commission.

"November 12, 1971."Includes bibliographical references (page 28)U.S. Atomic Energy Commission Contr...

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

Melson, N. Duane.
Keller, James D.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.

January 1983

"April 1983"--Cover.Distributed to depository libraries in microfiche.Includes bibliographical refer...

Reverse-flow combustor for small gas turbines with pressure-atomizing fuel injectors /

Norgren, Carl T.
Riddlebaugh, Stephen M., joint author.
Mularz, Edward J., joint author.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Office.

January 1978

Issued July 1978."AVRADCOM technical report 78-22(PL)."Includes bibliographical references.Mode of a...

Computation of three-dimensional nozzle-exhaust flow fields with the GIM code /

Spradley, L. W.
Pearson, M. L. (Marcus Lowell), 1941- joint author.
Anderson, P. G., joint author.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Office.

Issued Augt. 1978.Prepared for Langley Research Center, by Lockheed Missiles and Space Co., Inc., un...

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

Anderson, Bernhard H.
Lewis Research Center.

January 1974

Prepared at Lewis Research Center.Cover title.Includes bibliographical references (p. 83).Mode of ac...

A simplified computer program for the prediction of the linear stability behavior of liquid propellant combustors /

Mitchell, C. E.
Eckert, K.
Lewis Research Center.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.

January 1979

STAR category no. 20."August 1979"--Cover.Includes bibliographical references.Mode of access: Intern...

The AEDC three-dimensional, potential flow computer program.

Todd, Donald C., author.
ARO, Inc. sponsor.
United States. Air Force. Arnold Air Force Base. sponsor.
United States. Air Force. Systems Command. Arnold Engineering Development Center. issuing body.

"Program Element 65807.""Final Report for Period November 1971--November 1974.""February 1976."Inclu...

Combustion of hydrogen injected into a supersonic airstream (the ship computer program) /

Markatos, N. C.
Tatchell, D. G., joint author.
Spalding, D. B. (Dudley Brian), 1923- joint author.
Fluid Mechanics and Thermal Systems.
United States. National Aeronautics and Space Administration.

January 1977

Issued April 1977.Prepared by Fluid Mechanics and Thermal Systems, Inc. for Langley Research Center ...

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...

An improved supersonic, three-dimensional, external, inviscid flow field code /

Marconi, Frank.
Koch, Frank, 1931- joint author.
Grumman Aerospace Corporation.
Langley Research Center.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Office.

January 1979

March 1979.Prepared for Langley Research Center under contract NAS1-14162.Includes bibliographical r...

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

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

An approximate method for calculating three-dimensional inviscid hypersonic flow fields /

Riley, Christopher J. (Christopher Joseph), 1964-
DeJarnette, Fred R.
Langley Research Center.

January 1990

Prepared at Langley Research Center.Bibliography: p. 12.Mode of access: Internet

Investigations of three dimensional flow characteristics in a three bladed rocket pump inducer /

Poncet, A.
Lakshminarayana, B.
Lewis Research Center.
Pennsylvania State University.

January 1973

"Prepared by Pennsylvania State University ... for Lewis Research Center."Cover title.Bibliography: ...

Development of a three-dimensional turbulent duct flow analysis /

United States. National Aeronautics and Space Administration. Scientific and Technical Information Office.
Eiseman, P. R.
Lewis Research Center.
United Technologies Research Center.

January 1978

Nov. 1978.Contract NAS3-19856.Includes bibliographical references.Mode of access: Internet

Calculating three-dimensional flows around structures and over rough terrain /

Hirt, C. W.
Cook, J. L.
Los Alamos Scientific Laboratory.
U.S. Atomic Energy Commission.

"November 12, 1971."Includes bibliographical references (page 28)U.S. Atomic Energy Commission Contr...

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

Melson, N. Duane.
Keller, James D.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.

January 1983

"April 1983"--Cover.Distributed to depository libraries in microfiche.Includes bibliographical refer...

Reverse-flow combustor for small gas turbines with pressure-atomizing fuel injectors /

Norgren, Carl T.
Riddlebaugh, Stephen M., joint author.
Mularz, Edward J., joint author.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Office.

January 1978

Issued July 1978."AVRADCOM technical report 78-22(PL)."Includes bibliographical references.Mode of a...

Computation of three-dimensional nozzle-exhaust flow fields with the GIM code /

Spradley, L. W.
Pearson, M. L. (Marcus Lowell), 1941- joint author.
Anderson, P. G., joint author.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Office.

Issued Augt. 1978.Prepared for Langley Research Center, by Lockheed Missiles and Space Co., Inc., un...

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

Anderson, Bernhard H.
Lewis Research Center.

January 1974

Prepared at Lewis Research Center.Cover title.Includes bibliographical references (p. 83).Mode of ac...

A simplified computer program for the prediction of the linear stability behavior of liquid propellant combustors /

Mitchell, C. E.
Eckert, K.
Lewis Research Center.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.

January 1979

STAR category no. 20."August 1979"--Cover.Includes bibliographical references.Mode of access: Intern...

The development of a three-dimensional partially elliptic flow computer program for combustor research /

Abstract

Extracted data

The development of a three-dimensional partially elliptic flow computer program for combustor research /

Abstract

Extracted data

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