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

FORTRAN program for calculating coolant flow and metal temperatures of a full-coverage-film-cooled vane or blade /

Meitner, Peter L.
Propulsion Laboratory (U.S.)
United States. National Aeronautics and Space Administration. Scientific and Technical Information Office.

January 1978

July 1978.AVRADCOM technical report 78-19(PL).Includes bibliographical references.Mode of access: In...

Revised FORTRAN program for calculating velocities and streamlines on the hub-shroud midchannel stream surface of an axial-, radial-, or mixed-flow turbomachine or annular duct /

Katsanis, Theodore.
McNally, William D.
Lewis Research Center.

January 1977

"Lewis Research Center."Supersedes NASA TN D-7343.Cover title.Bibliography: p. 101-102, v. 1.1. User...

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

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

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

A Fortran IV program to estimate the off-design performance of radial-inflow turbines /

Todd, Carroll A.
Futral, Samuel M.
Lewis Research Center.

Prepared at Lewis Research Center."March 1969"--Cover.Includes bibliographical references (p. 47).Mo...

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...

FORTRAN program for predicting off-design performance of centrifugal compressors /

Galvas, Michael R.
U.S. Army Air Mobility Research and Development Laboratory.
Lewis Research Center.

January 1973

Prepared at Lewis Research Center and the U.S. Army Air Mobility R&D Laboratory.Cover title.Includes...

Numerical method for predicting flow characteristics and performance of nonaxisymmetric nozzles : part 2 - applications /

Thomas, P. D. (Paul Denis), 1935-
Langley Research Center.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.

January 1980

"Contract NAS1-15084."Oct. 1980.Includes bibliographical references.Mode of access: Internet

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...

Static performance of an axisymmetric nozzle with post-exit vanes for multiaxis thrust vectoring /

Berrier, Bobby L.
Langley Research Center.

January 1988

Prepared at Langley Research Center."May 1988"--Cover.Includes bibliographical references (p. 11).Mo...

Static performance of nonaxisymmetric nozzles with yaw thrust-vectoring vanes /

Mason, Mary L.
Berrier, Bobby L.
Langley Research Center.

January 1988

Prepared at Langley Research Center."May 1988"--Cover.Includes bibliographical references (p. 10).Mo...

Numerical calculations for the characteristics of a gas flowing axially through a constricted arc /

Watson, Velvin R. (Velvin Richard)
Pegot, Eva B.
United States. National Aeronautics and Space Administration.
Ames Research Center.

Prepared at Ames Research Center."June 1967"--Cover.Includes bibliographical references (p. 117).Mod...

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...

Charts for equilibrium flow properties of air in hypervelocity nozzles /

Jorgensen, Leland H.
Baum, Geyle M.
Ames Research Center.

Prepared at Ames Research Center."September 1962."Cover title.Includes bibliographical references (p...

FORTRAN program for calculating coolant flow and metal temperatures of a full-coverage-film-cooled vane or blade /

Meitner, Peter L.
Propulsion Laboratory (U.S.)
United States. National Aeronautics and Space Administration. Scientific and Technical Information Office.

January 1978

July 1978.AVRADCOM technical report 78-19(PL).Includes bibliographical references.Mode of access: In...

Revised FORTRAN program for calculating velocities and streamlines on the hub-shroud midchannel stream surface of an axial-, radial-, or mixed-flow turbomachine or annular duct /

Katsanis, Theodore.
McNally, William D.
Lewis Research Center.

January 1977

"Lewis Research Center."Supersedes NASA TN D-7343.Cover title.Bibliography: p. 101-102, v. 1.1. User...

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

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

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

A Fortran IV program to estimate the off-design performance of radial-inflow turbines /

Todd, Carroll A.
Futral, Samuel M.
Lewis Research Center.

Prepared at Lewis Research Center."March 1969"--Cover.Includes bibliographical references (p. 47).Mo...

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...

FORTRAN program for predicting off-design performance of centrifugal compressors /

Galvas, Michael R.
U.S. Army Air Mobility Research and Development Laboratory.
Lewis Research Center.

January 1973

Prepared at Lewis Research Center and the U.S. Army Air Mobility R&D Laboratory.Cover title.Includes...

Numerical method for predicting flow characteristics and performance of nonaxisymmetric nozzles : part 2 - applications /

Thomas, P. D. (Paul Denis), 1935-
Langley Research Center.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.

January 1980

"Contract NAS1-15084."Oct. 1980.Includes bibliographical references.Mode of access: Internet

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...

Static performance of an axisymmetric nozzle with post-exit vanes for multiaxis thrust vectoring /

Berrier, Bobby L.
Langley Research Center.

January 1988

Prepared at Langley Research Center."May 1988"--Cover.Includes bibliographical references (p. 11).Mo...

Static performance of nonaxisymmetric nozzles with yaw thrust-vectoring vanes /

Mason, Mary L.
Berrier, Bobby L.
Langley Research Center.

January 1988

Prepared at Langley Research Center."May 1988"--Cover.Includes bibliographical references (p. 10).Mo...

Numerical calculations for the characteristics of a gas flowing axially through a constricted arc /

Watson, Velvin R. (Velvin Richard)
Pegot, Eva B.
United States. National Aeronautics and Space Administration.
Ames Research Center.

Prepared at Ames Research Center."June 1967"--Cover.Includes bibliographical references (p. 117).Mod...

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...

Charts for equilibrium flow properties of air in hypervelocity nozzles /

Jorgensen, Leland H.
Baum, Geyle M.
Ames Research Center.

Prepared at Ames Research Center."September 1962."Cover title.Includes bibliographical references (p...

FORTRAN program for calculating coolant flow and metal temperatures of a full-coverage-film-cooled vane or blade /

Meitner, Peter L.
Propulsion Laboratory (U.S.)
United States. National Aeronautics and Space Administration. Scientific and Technical Information Office.

January 1978

July 1978.AVRADCOM technical report 78-19(PL).Includes bibliographical references.Mode of access: In...

Revised FORTRAN program for calculating velocities and streamlines on the hub-shroud midchannel stream surface of an axial-, radial-, or mixed-flow turbomachine or annular duct /

Katsanis, Theodore.
McNally, William D.
Lewis Research Center.

January 1977

"Lewis Research Center."Supersedes NASA TN D-7343.Cover title.Bibliography: p. 101-102, v. 1.1. User...

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

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

Abstract

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

Abstract

Extracted data

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