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

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...

Fortran IV computer program for calculating critical speeds of rotating shafts /

Trivisonno, Roger J.
Lewis Research Center.

January 1973

Prepared at Lewis Research Center.Cover title.Includes bibliographical references (p. 52).Mode of ac...

Computer program for aerodynamic and blading design of multistage axial-flow compressors /

Crouse, James E.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.
Lewis Research Center.

January 1981

STAR Category 07."Lewis Research Center.""December 1981"--Cover."Propulsion Laboratory, AVRADCOM Res...

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

Improved method for calculating transonic velocities on blade-to-blade stream surfaces of a turbomachine /

Wood, Jerry R.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.
Lewis Research Center.

January 1981

STAR category 02."April 1981"--Cover."Lewis Research Center."Includes bibliographical references.Mod...

WIND : computer program for calculation of three-dimensional potential compressible flow about wind turbine rotor blades /

Dulikravich, Djordje S.
Lewis Research Center.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.

January 1980

Oct. 1980."Lewis Research Center."Includes bibliographical references.Mode of access: Internet

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 generating input for analysis of impingement-cooled, axial-flow turbine blade /

Rosenbaum, David.
Lewis Research Center.
Army Research and Technology Laboratories (U.S.). Structures Laboratory.
Propulsion Laboratory (U.S.)
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.

January 1980

STAR category 34."January 1980"--Cover.Distributed to depository libraries in microfiche."Propulsion...

Computer program for design-point performance of turbojet and turbofan engine cycles /

Vanco, Michael R.
Lewis Research Center.

January 1967

"NASA TM X-1340.""Lewis Research Center, Cleveland, Ohio.""February 1967"--Cover.Includes bibliograp...

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...

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

FORTRAN program for calculating velocities and streamlines on a blade-to-blade stream surface of a tandem blade turbomachine /

Katsanis, Theodore.
McNally, William D.
Lewis Research Center.
United States. National Aeronautics and Space Administration.

Cover title."March 1969."Includes bibliographical references (p. 108-109).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...

A quasi-three-dimensional method for calculating blade surface velocities for an axial flow turbine blade /

Katsanis, Theodore.
Dellner, Lois T.
Lewis Research Center.

January 1967

"NASA TM X-1394.""Lewis Research Center, Cleveland, Ohio.""June 1967"--Cover.Includes bibliographica...

A FORTRAN program for calculating three-dimensional, inviscid, rotational flows with shock waves in axial compressor blade rows : user's manual /

Thompkins, William T.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Office.
Gas Turbine and Plasma Dynamics Laboratory.
Lewis Research Center.

January 1982

STAR category 02."June 1982"--Cover."Massachusetts Institute of Technology, Gas Turbine and Plasma D...

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...

Fortran IV computer program for calculating critical speeds of rotating shafts /

Trivisonno, Roger J.
Lewis Research Center.

January 1973

Prepared at Lewis Research Center.Cover title.Includes bibliographical references (p. 52).Mode of ac...

Computer program for aerodynamic and blading design of multistage axial-flow compressors /

Crouse, James E.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.
Lewis Research Center.

January 1981

STAR Category 07."Lewis Research Center.""December 1981"--Cover."Propulsion Laboratory, AVRADCOM Res...

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

Improved method for calculating transonic velocities on blade-to-blade stream surfaces of a turbomachine /

Wood, Jerry R.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.
Lewis Research Center.

January 1981

STAR category 02."April 1981"--Cover."Lewis Research Center."Includes bibliographical references.Mod...

WIND : computer program for calculation of three-dimensional potential compressible flow about wind turbine rotor blades /

Dulikravich, Djordje S.
Lewis Research Center.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.

January 1980

Oct. 1980."Lewis Research Center."Includes bibliographical references.Mode of access: Internet

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 generating input for analysis of impingement-cooled, axial-flow turbine blade /

Rosenbaum, David.
Lewis Research Center.
Army Research and Technology Laboratories (U.S.). Structures Laboratory.
Propulsion Laboratory (U.S.)
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.

January 1980

STAR category 34."January 1980"--Cover.Distributed to depository libraries in microfiche."Propulsion...

Computer program for design-point performance of turbojet and turbofan engine cycles /

Vanco, Michael R.
Lewis Research Center.

January 1967

"NASA TM X-1340.""Lewis Research Center, Cleveland, Ohio.""February 1967"--Cover.Includes bibliograp...

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...

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

FORTRAN program for calculating velocities and streamlines on a blade-to-blade stream surface of a tandem blade turbomachine /

Katsanis, Theodore.
McNally, William D.
Lewis Research Center.
United States. National Aeronautics and Space Administration.

Cover title."March 1969."Includes bibliographical references (p. 108-109).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...

A quasi-three-dimensional method for calculating blade surface velocities for an axial flow turbine blade /

Katsanis, Theodore.
Dellner, Lois T.
Lewis Research Center.

January 1967

"NASA TM X-1394.""Lewis Research Center, Cleveland, Ohio.""June 1967"--Cover.Includes bibliographica...

A FORTRAN program for calculating three-dimensional, inviscid, rotational flows with shock waves in axial compressor blade rows : user's manual /

Thompkins, William T.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Office.
Gas Turbine and Plasma Dynamics Laboratory.
Lewis Research Center.

January 1982

STAR category 02."June 1982"--Cover."Massachusetts Institute of Technology, Gas Turbine and Plasma D...

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...

Fortran IV computer program for calculating critical speeds of rotating shafts /

Trivisonno, Roger J.
Lewis Research Center.

January 1973

Prepared at Lewis Research Center.Cover title.Includes bibliographical references (p. 52).Mode of ac...

Computer program for aerodynamic and blading design of multistage axial-flow compressors /

Crouse, James E.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.
Lewis Research Center.

January 1981

STAR Category 07."Lewis Research Center.""December 1981"--Cover."Propulsion Laboratory, AVRADCOM Res...

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

Abstract

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

Abstract

Extracted data

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