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

Real-time simulation of the TF30-P-3 turbofan engine using a hybrid computer /

Szuch, John R.
Bruton, William M.
Lewis Research Center.

January 1974

Prepared at Lewis Research Center.Cover title.Includes bibliographical references (p. 54).Mode of ac...

An experimental investigation of an advanced turboprop installation on a swept wing at subsonic and transonic speeds /

Carlson, John R.
Pendergraft, Odis C.
Langley Research Center.

January 1987

"September 1987"--Cover.Prepared at Langley Research Center.Includes bibliographical references (p. ...

A computer program for calculating model planetary atmospheres /

Pitts, David E.
Manned Spacecraft Center (U.S.)

Prepared at Manned Spacecraft Center."February 1968"--Cover.Includes bibliographical references (p. ...

Computer program for thermodynamic performance of Brayton-cycle space-power systems /

Glassman, Arthur J.
Lewis Research Center.

January 1967

"NASA TM X-1339.""Lewis Research Center, Cleveland, Ohio.""January 1967"--Cover.Includes bibliograph...

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...

Computer program for estimating performance of air-breathing aircraft engines /

Geiselhart, Karl A.
Morris, Shelby J.
Caddy, Michael J.
Langley Research Center.

January 1991

Prepared at Langley Research Center.Bibliography: p. 128.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...

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...

DYNGEN : a program for calculating steady-state and transient performance of turbojet and turbofan engines /

Sellers, James F.
Daniele, Carl J.
United States. National Aeronautics and Space Administration.

January 1975

"April 1975."Cover title.Includes bibliographical references (p. 179).Mode of access: Internet

Performance of a turbojet engine in combination with an external-internal-compression inlet to mach 2.88 /

Bowditch, David N.
Tabata, William K.
Anderson, Bernhard H.
United States. National Aeronautics and Space Administration.

"July 1960."Cover title.Includes bibliographical references (p. 10-11).Mode of access: Internet

A computer program for wing subsonic aerodynamic performance estimates including attainable thrust and vortex lift effects /

Carlson, Harry W.
Walkley, Kenneth B.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.
Langley Research Center.

January 1982

Subject Category 01."March 1982"--Cover.Includes bibliographical references.Mode of access: Internet

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...

A computer program for calculating design and off-design performance of two- and three-spool turbofans with as many as three nozzles

Fishbach, L. H.
Koenig, R. W.

November 1973

Program uses component performance maps to enable user to do analytical engine cycle calculations. E...

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...

Turbojet combustor performance with natural gas fuel

Marchionna, Nicholas R.
Trout, Arthur M.
United States. National Aeronautics and Space Administration.
Lewis Research Center.

Prepared at Lewis Research Center."February 1970."Cover title.Includes bibliographical references (p...

Real-time simulation of the TF30-P-3 turbofan engine using a hybrid computer /

Szuch, John R.
Bruton, William M.
Lewis Research Center.

January 1974

Prepared at Lewis Research Center.Cover title.Includes bibliographical references (p. 54).Mode of ac...

An experimental investigation of an advanced turboprop installation on a swept wing at subsonic and transonic speeds /

Carlson, John R.
Pendergraft, Odis C.
Langley Research Center.

January 1987

"September 1987"--Cover.Prepared at Langley Research Center.Includes bibliographical references (p. ...

A computer program for calculating model planetary atmospheres /

Pitts, David E.
Manned Spacecraft Center (U.S.)

Prepared at Manned Spacecraft Center."February 1968"--Cover.Includes bibliographical references (p. ...

Computer program for thermodynamic performance of Brayton-cycle space-power systems /

Glassman, Arthur J.
Lewis Research Center.

January 1967

"NASA TM X-1339.""Lewis Research Center, Cleveland, Ohio.""January 1967"--Cover.Includes bibliograph...

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...

Computer program for estimating performance of air-breathing aircraft engines /

Geiselhart, Karl A.
Morris, Shelby J.
Caddy, Michael J.
Langley Research Center.

January 1991

Prepared at Langley Research Center.Bibliography: p. 128.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...

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...

DYNGEN : a program for calculating steady-state and transient performance of turbojet and turbofan engines /

Sellers, James F.
Daniele, Carl J.
United States. National Aeronautics and Space Administration.

January 1975

"April 1975."Cover title.Includes bibliographical references (p. 179).Mode of access: Internet

Performance of a turbojet engine in combination with an external-internal-compression inlet to mach 2.88 /

Bowditch, David N.
Tabata, William K.
Anderson, Bernhard H.
United States. National Aeronautics and Space Administration.

"July 1960."Cover title.Includes bibliographical references (p. 10-11).Mode of access: Internet

A computer program for wing subsonic aerodynamic performance estimates including attainable thrust and vortex lift effects /

Carlson, Harry W.
Walkley, Kenneth B.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.
Langley Research Center.

January 1982

Subject Category 01."March 1982"--Cover.Includes bibliographical references.Mode of access: Internet

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...

A computer program for calculating design and off-design performance of two- and three-spool turbofans with as many as three nozzles

Fishbach, L. H.
Koenig, R. W.

November 1973

Program uses component performance maps to enable user to do analytical engine cycle calculations. E...

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...

Turbojet combustor performance with natural gas fuel

Marchionna, Nicholas R.
Trout, Arthur M.
United States. National Aeronautics and Space Administration.
Lewis Research Center.

Prepared at Lewis Research Center."February 1970."Cover title.Includes bibliographical references (p...

Real-time simulation of the TF30-P-3 turbofan engine using a hybrid computer /

Szuch, John R.
Bruton, William M.
Lewis Research Center.

January 1974

Prepared at Lewis Research Center.Cover title.Includes bibliographical references (p. 54).Mode of ac...

An experimental investigation of an advanced turboprop installation on a swept wing at subsonic and transonic speeds /

Carlson, John R.
Pendergraft, Odis C.
Langley Research Center.

January 1987

"September 1987"--Cover.Prepared at Langley Research Center.Includes bibliographical references (p. ...

A computer program for calculating model planetary atmospheres /

Pitts, David E.
Manned Spacecraft Center (U.S.)

Prepared at Manned Spacecraft Center."February 1968"--Cover.Includes bibliographical references (p. ...

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

Abstract

Extracted data

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

Abstract

Extracted data

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