Computer code for off-design performance analysis of radial-inflow turbines with rotor blade sweep /

Off-design performance loss model for radial turbines with pivoting, variable-area stators /

Meitner, Peter L.
Glassman, Arthur J.
Propulsion Laboratory (U.S.)
Lewis Research Center.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.

January 1980

Nov. 1980."Lewis Research Center.""Propulsion Laboratory."Includes bibliographical references.Mode o...

Review and status of heat-transfer technology for internal passages of air-cooled turbine blades /

Yeh, Frederick C.
Stepka, Francis S.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.

January 1984

STAR category 34."April 1984"--Cover.Distributed to depository libraries in microfiche.Includes bibl...

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...

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...

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...

Experimental results of varying the blade-shroud clearance in a 6.02-inch radial-inflow turbine /

Futral, Samuel M.
Holeski, Donald E.

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

Analysis of a topping-cycle, aircraft, gas-turbine-engine system which uses cryogenic fuel /

Turney, George E.
Fishbach, Laurence H.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.

January 1984

STAR category 07."April 1984"--Cover.Distributed to depository libraries in microfiche.Includes bibl...

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 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...

Incidence loss for fan turbine rotor blade in two-dimensional cascade /

Kline, John F.
Stabe, Roy G.
Moffitt, Thomas P.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.
Lewis Research Center.

January 1983

STAR category 07."July 1983"--Cover.Distributed to depository libraries in microfiche."Lewis Researc...

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

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...

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

Off-design performance loss model for radial turbines with pivoting, variable-area stators /

Meitner, Peter L.
Glassman, Arthur J.
Propulsion Laboratory (U.S.)
Lewis Research Center.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.

January 1980

Nov. 1980."Lewis Research Center.""Propulsion Laboratory."Includes bibliographical references.Mode o...

Review and status of heat-transfer technology for internal passages of air-cooled turbine blades /

Yeh, Frederick C.
Stepka, Francis S.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.

January 1984

STAR category 34."April 1984"--Cover.Distributed to depository libraries in microfiche.Includes bibl...

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...

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...

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...

Experimental results of varying the blade-shroud clearance in a 6.02-inch radial-inflow turbine /

Futral, Samuel M.
Holeski, Donald E.

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

Analysis of a topping-cycle, aircraft, gas-turbine-engine system which uses cryogenic fuel /

Turney, George E.
Fishbach, Laurence H.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.

January 1984

STAR category 07."April 1984"--Cover.Distributed to depository libraries in microfiche.Includes bibl...

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 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...

Incidence loss for fan turbine rotor blade in two-dimensional cascade /

Kline, John F.
Stabe, Roy G.
Moffitt, Thomas P.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.
Lewis Research Center.

January 1983

STAR category 07."July 1983"--Cover.Distributed to depository libraries in microfiche."Lewis Researc...

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

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...

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

Off-design performance loss model for radial turbines with pivoting, variable-area stators /

Meitner, Peter L.
Glassman, Arthur J.
Propulsion Laboratory (U.S.)
Lewis Research Center.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.

January 1980

Nov. 1980."Lewis Research Center.""Propulsion Laboratory."Includes bibliographical references.Mode o...

Review and status of heat-transfer technology for internal passages of air-cooled turbine blades /

Yeh, Frederick C.
Stepka, Francis S.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.

January 1984

STAR category 34."April 1984"--Cover.Distributed to depository libraries in microfiche.Includes bibl...

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

Computer code for off-design performance analysis of radial-inflow turbines with rotor blade sweep /

Abstract

Extracted data

Computer code for off-design performance analysis of radial-inflow turbines with rotor blade sweep /

Abstract

Extracted data

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