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

Analysis of factors affecting selection and design of air-cooled single-stage turbines for turbojet engines

Hubbartt, James E.
Schramm, Wilson B., joint author.
Rossbach, Richard J., joint author.
United States. National Advisory Committee for Aeronautics. NACA research memorandum.
Lewis Flight Propulsion Laboratory.

On front cover: "September 16, 1954."Title from cover.Includes bibliographical references: p. 24.Mod...

Analysis of thermal-protection systems for space-vehicle cryogenic-propellant tanks /

Smolak, George R.
Wallner, Lewis E.
Knoll, Richard H.
United States. National Aeronautics and Space Administration.
Lewis Research Center.

January 1962

"Advance Copy."Includes bibliographical references (p. 68-70).Mode of access: Internet

150 and 300 kW lightweight diesel aircraft engine study /

Brouwers, Alex P.
Lewis Research Center.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Office.

January 1980

Subject category 07."April 1980"--Cover.Bibliography: p. 132-142.Mode of access: Internet

Analysis of potential benefits of integrated-gasifier combined cycles for a utility system /

Choo, Yung K.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.

January 1983

STAR category 44."October 1983"--Cover.Distributed to depository libraries in microfiche.Includes bi...

Recent trends in aviation turbine fuel properties /

Friedman, Robert, 1929-
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.
Lewis Research Center.

January 1982

STAR category 28."October 1982"--Cover.Includes bibliographical references.Mode of access: Internet

Aviation turbine fuels, 1975 /

Shelton, E. M. (Ella Mae) author.
Bartlesville Energy Research Center.
American Petroleum Institute.
Pittsburgh Energy Research Center.
United States. Energy Research and Development Administration.

Published March 1976.Includes bibliographical references.Mode of access: Internet

Integrated exhaust gas analysis system for aircraft turbine engine component testing /

Summers, Robert L.
Anderson, Robert C. (Robert Charles), 1943-
Lewis Research Center.

January 1985

Prepared at Lewis Research Center."January 1985"--Cover.Includes bibliographical references (p. 25)....

Analysis and selection of design conditions for a radioisotope brayton-cycle space powerplant /

Klann, John L.
Lewis Research Center.
United States. National Aeronautics and Space Administration.

January 1968

Cover title."June 1968."Includes bibliographical references (p. 79-80).Mode of access: Internet

Analysis of topping and bleed turbopump units for hydrogen-propelled nuclear rockets /

Evans, David G.
Crouse, James E.
Lewis Research Center.

January 1960

"June 1960."Cover title.Includes bibliographical references (p. 24).Mode of access: Internet

Cold-air performance evaluation of scale model oxidizer pump-drive turbine for the M-1 hydrogen-oxygen rocket engine.

Stabe, Roy G.
Kline, John F.
Lewis Research Center.
United States. National Aeronautics and Space Administration.

January 1968

Cover title."February 1968."Includes bibliographical references (p. 20-21).Mode of access: Internet

Design analysis of a subsonic nuclear-powered logistic airplane with helium-cooled reactor /

Cavicchi, R. H.
United States. National Aeronautics and Space Administration.

"October 23, 1959."Cover title.Includes bibliographical references (p. 161-164).Mode of access: Inte...

Thermal analysis of a planetary transmission with spherical roller bearings operating after complete loss of oil /

Coe, Harold H.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.

January 1984

Distributed to depository libraries in microfiche."September 1984"--Cover.Includes bibliographical r...

Cold-air investigation of prototype Snap-8 turbine

Nusbaum, William J.
Holeski, Donald E.
United States. National Aeronautics and Space Administration.

Cover title."October 1962."Fluid mechanics;Power sources, supplementary; Propulsion system elements;...

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...

Dilution-jet mixing study for gas-turbine combustors /

Norgren, Carl T.
Humenik, Francis M.
United States. National Aeronautics and Space Administration.

Cover title."August 1968."Includes bibliographical references.Mode of access: Internet

Analysis of factors affecting selection and design of air-cooled single-stage turbines for turbojet engines

Hubbartt, James E.
Schramm, Wilson B., joint author.
Rossbach, Richard J., joint author.
United States. National Advisory Committee for Aeronautics. NACA research memorandum.
Lewis Flight Propulsion Laboratory.

On front cover: "September 16, 1954."Title from cover.Includes bibliographical references: p. 24.Mod...

Analysis of thermal-protection systems for space-vehicle cryogenic-propellant tanks /

Smolak, George R.
Wallner, Lewis E.
Knoll, Richard H.
United States. National Aeronautics and Space Administration.
Lewis Research Center.

January 1962

"Advance Copy."Includes bibliographical references (p. 68-70).Mode of access: Internet

150 and 300 kW lightweight diesel aircraft engine study /

Brouwers, Alex P.
Lewis Research Center.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Office.

January 1980

Subject category 07."April 1980"--Cover.Bibliography: p. 132-142.Mode of access: Internet

Analysis of potential benefits of integrated-gasifier combined cycles for a utility system /

Choo, Yung K.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.

January 1983

STAR category 44."October 1983"--Cover.Distributed to depository libraries in microfiche.Includes bi...

Recent trends in aviation turbine fuel properties /

Friedman, Robert, 1929-
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.
Lewis Research Center.

January 1982

STAR category 28."October 1982"--Cover.Includes bibliographical references.Mode of access: Internet

Aviation turbine fuels, 1975 /

Shelton, E. M. (Ella Mae) author.
Bartlesville Energy Research Center.
American Petroleum Institute.
Pittsburgh Energy Research Center.
United States. Energy Research and Development Administration.

Published March 1976.Includes bibliographical references.Mode of access: Internet

Integrated exhaust gas analysis system for aircraft turbine engine component testing /

Summers, Robert L.
Anderson, Robert C. (Robert Charles), 1943-
Lewis Research Center.

January 1985

Prepared at Lewis Research Center."January 1985"--Cover.Includes bibliographical references (p. 25)....

Analysis and selection of design conditions for a radioisotope brayton-cycle space powerplant /

Klann, John L.
Lewis Research Center.
United States. National Aeronautics and Space Administration.

January 1968

Cover title."June 1968."Includes bibliographical references (p. 79-80).Mode of access: Internet

Analysis of topping and bleed turbopump units for hydrogen-propelled nuclear rockets /

Evans, David G.
Crouse, James E.
Lewis Research Center.

January 1960

"June 1960."Cover title.Includes bibliographical references (p. 24).Mode of access: Internet

Cold-air performance evaluation of scale model oxidizer pump-drive turbine for the M-1 hydrogen-oxygen rocket engine.

Stabe, Roy G.
Kline, John F.
Lewis Research Center.
United States. National Aeronautics and Space Administration.

January 1968

Cover title."February 1968."Includes bibliographical references (p. 20-21).Mode of access: Internet

Design analysis of a subsonic nuclear-powered logistic airplane with helium-cooled reactor /

Cavicchi, R. H.
United States. National Aeronautics and Space Administration.

"October 23, 1959."Cover title.Includes bibliographical references (p. 161-164).Mode of access: Inte...

Thermal analysis of a planetary transmission with spherical roller bearings operating after complete loss of oil /

Coe, Harold H.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.

January 1984

Distributed to depository libraries in microfiche."September 1984"--Cover.Includes bibliographical r...

Cold-air investigation of prototype Snap-8 turbine

Nusbaum, William J.
Holeski, Donald E.
United States. National Aeronautics and Space Administration.

Cover title."October 1962."Fluid mechanics;Power sources, supplementary; Propulsion system elements;...

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...

Dilution-jet mixing study for gas-turbine combustors /

Norgren, Carl T.
Humenik, Francis M.
United States. National Aeronautics and Space Administration.

Cover title."August 1968."Includes bibliographical references.Mode of access: Internet

Analysis of factors affecting selection and design of air-cooled single-stage turbines for turbojet engines

Hubbartt, James E.
Schramm, Wilson B., joint author.
Rossbach, Richard J., joint author.
United States. National Advisory Committee for Aeronautics. NACA research memorandum.
Lewis Flight Propulsion Laboratory.

On front cover: "September 16, 1954."Title from cover.Includes bibliographical references: p. 24.Mod...

Analysis of thermal-protection systems for space-vehicle cryogenic-propellant tanks /

Smolak, George R.
Wallner, Lewis E.
Knoll, Richard H.
United States. National Aeronautics and Space Administration.
Lewis Research Center.

January 1962

"Advance Copy."Includes bibliographical references (p. 68-70).Mode of access: Internet

150 and 300 kW lightweight diesel aircraft engine study /

Brouwers, Alex P.
Lewis Research Center.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Office.

January 1980

Subject category 07."April 1980"--Cover.Bibliography: p. 132-142.Mode of access: Internet

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

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

Abstract

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