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

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 code for predicting coolant flow and heat transfer in turbomachinery /

Meitner, Peter L.
United States. Army Aviation Systems Command. Propulsion Directorate.
Lewis Research Center.

January 1990

Prepared at Lewis Research Center and the Propulsion Directorate, U.S. Army Aviation Systems Command...

A computer program to predict rotor rotational noise of a stationary rotor from blade loading coefficients /

Ramakrishnan, Ramani.
Hosier, Robert N., joint author.
Randall, Donald, joint author.
Langley Research Center.

January 1976

Cover title.Includes bibliographical references (p. 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...

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...

FORTRAN program for induction motor analysis /

Bollenbacher, Gary.
Lewis Research Center.

January 1976

Cover title.Includes bibliographical references (p. 70).Mode of access: Internet

A FORTRAN program for determining aircraft stability and control derivatives from flight data /

Maine, Richard E.
Iliff, Kenneth W.
Flight Research Center (U.S.)

January 1975

Prepared at the NASA Flight Research Center.Cover title.Includes bibliographical references (p. 171)...

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

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...

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

Method for predicting off-design performance of axial-flow compressor blade rows /

Serovy, G. K. (George K.)
Anderson, E. W.
Iowa State College.

January 1959

"NASA TN D-110.""Iowa State College.""August 1959."Title from cover.Includes bibliographical referen...

FORTRAN program to generate engine inlet flow contour maps and distortion parameters /

Dicus, John H.
Lewis Research Center.

January 1974

Prepared at Lewis Research Center.Cover title.Includes bibliographical references (p. 61).Mode of ac...

Performance of inlet stage of transonic compressor /

Urasek, Donald C.
Lewis, George W., Jr.
Steinke, Ronald J.
Lewis Research Center.

January 1976

Prepared at Lewis Research Center.Cover title.Includes bibliographical references (p. 17).Mode of ac...

An analytical method for predicting the performance of centrifugal pumps during pressurized startup /

Rostafiński, Wojciech.
United States. National Aeronautics and Space Administration.
Lewis Research Center.

Prepared at Lewis Research Center."January 1969"--Cover.Includes bibliographical references (p. 37)....

Calculations of the performance of a compression-ignition engine-compressor turbine combination.

Mendelson, Alexander.
United States. National Advisory Committee for Aeronautics. NACA research memorandum.
Aircraft Engine Research Laboratory.

Prepared at the Aircraft Engine Research Laboratory, Cleveland, Ohio.On front cover: "February 3, 19...

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 code for predicting coolant flow and heat transfer in turbomachinery /

Meitner, Peter L.
United States. Army Aviation Systems Command. Propulsion Directorate.
Lewis Research Center.

January 1990

Prepared at Lewis Research Center and the Propulsion Directorate, U.S. Army Aviation Systems Command...

A computer program to predict rotor rotational noise of a stationary rotor from blade loading coefficients /

Ramakrishnan, Ramani.
Hosier, Robert N., joint author.
Randall, Donald, joint author.
Langley Research Center.

January 1976

Cover title.Includes bibliographical references (p. 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...

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...

FORTRAN program for induction motor analysis /

Bollenbacher, Gary.
Lewis Research Center.

January 1976

Cover title.Includes bibliographical references (p. 70).Mode of access: Internet

A FORTRAN program for determining aircraft stability and control derivatives from flight data /

Maine, Richard E.
Iliff, Kenneth W.
Flight Research Center (U.S.)

January 1975

Prepared at the NASA Flight Research Center.Cover title.Includes bibliographical references (p. 171)...

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

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...

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

Method for predicting off-design performance of axial-flow compressor blade rows /

Serovy, G. K. (George K.)
Anderson, E. W.
Iowa State College.

January 1959

"NASA TN D-110.""Iowa State College.""August 1959."Title from cover.Includes bibliographical referen...

FORTRAN program to generate engine inlet flow contour maps and distortion parameters /

Dicus, John H.
Lewis Research Center.

January 1974

Prepared at Lewis Research Center.Cover title.Includes bibliographical references (p. 61).Mode of ac...

Performance of inlet stage of transonic compressor /

Urasek, Donald C.
Lewis, George W., Jr.
Steinke, Ronald J.
Lewis Research Center.

January 1976

Prepared at Lewis Research Center.Cover title.Includes bibliographical references (p. 17).Mode of ac...

An analytical method for predicting the performance of centrifugal pumps during pressurized startup /

Rostafiński, Wojciech.
United States. National Aeronautics and Space Administration.
Lewis Research Center.

Prepared at Lewis Research Center."January 1969"--Cover.Includes bibliographical references (p. 37)....

Calculations of the performance of a compression-ignition engine-compressor turbine combination.

Mendelson, Alexander.
United States. National Advisory Committee for Aeronautics. NACA research memorandum.
Aircraft Engine Research Laboratory.

Prepared at the Aircraft Engine Research Laboratory, Cleveland, Ohio.On front cover: "February 3, 19...

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 code for predicting coolant flow and heat transfer in turbomachinery /

Meitner, Peter L.
United States. Army Aviation Systems Command. Propulsion Directorate.
Lewis Research Center.

January 1990

Prepared at Lewis Research Center and the Propulsion Directorate, U.S. Army Aviation Systems Command...

A computer program to predict rotor rotational noise of a stationary rotor from blade loading coefficients /

Ramakrishnan, Ramani.
Hosier, Robert N., joint author.
Randall, Donald, joint author.
Langley Research Center.

January 1976

Cover title.Includes bibliographical references (p. 109).Mode of access: Internet

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

Abstract

Extracted data

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

Abstract

Extracted data

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