Performance of a turboalternator gas-bearing system at steady-state conditions /

Reduction of apparent-power requirement of phase-controlled parasitically loaded turboalternator by multiple parasitic loads /

Gilbert, Leonard J.
Lewis Research Center.

Prepared at Lewis Research Center."February 1968"--Cover.Includes bibliographical references (p. 34)...

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...

Effect of pressure ratio and inlet pressure on performance of experimental gas turbine at inlet temperature of 800©� R /

Kohl, Robert C.
Larkin, Robert G., joint author.
United States. National Advisory Committee for Aeronautics. NACA research memorandum.
Lewis Flight Propulsion Laboratory.

On front cover: "November 2, 1948."Includes bibliographical references: p. 4.Mode of access: Interne...

Transient performance of a turboalternator gas-bearing system /

Wood, James C.
Asadourian, Armen S.
Curreri, Joseph S.
Lewis Research Center.
United States. National Aeronautics and Space Administration.

January 1970

Experimental operation of gas-bearing turboalternator for spacecraft power supplies.Includes bibliog...

Steady-state electrical performance of a 400-Hertz Brayton cycle turboalternator and controls /

Valgora, Martin E.
Perz, Dennis A.
United States. National Aeronautics and Space Administration.
Lewis Research Center.

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

Turbine performance in a gas-bearing Brayton cycle turboalternator /

Curreri, Joseph S.
Wood, James C.
Kruchowy, Roman.
Lewis Research Center.
United States. National Aeronautics and Space Administration.

January 1969

Turbine performance in gas-bearing Brayton cycle turboalternator.Includes bibliographical references...

Static parasitic speed controller for Brayton-cycle turboalternator /

Word, John L.
Ingle, Bill D.
Fischer, Raymond L. E.
Lewis Research Center.

Prepared at Lewis Research Center."September 1967"--Cover.Includes bibliographical references (p. 13...

Static sea-level performance of an axial-flow-compressor turbojet engine with an air-cooled turbine /

Cochran, Reeves P.
Dengler, Robert P.
Cochran, Reeves P.
Lewis Flight Propulsion Laboratory.
United States. National Adviosry Committee for Aeronautics. NACA research memorandum.
United States. National Advisory Committee for Aeronautics.

"Declassified February 10, 1959.""March 15, 1955."Cover title.Includes bibliographical references (p...

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...

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...

Steady-state performance of a modified Rankine cycle system using water /

Fenn, David B.
Gutierrez, Orlando A.
Coe, Harold H.
Lewis Research Center.

Prepared at Lewis Research Center."March 1966"--Cover.Includes bibliographical references (p. 18).Mo...

Experimental evaluation of volt-ampere loading and output distortion for a turboalternator with multiple load phase-controlled parasitic speed controller /

Perz, Dennis A.
Valgora, Martin E.
Lewis Research Center.

Prepared at Lewis Research Center."December 1969."Cover title.Includes bibliographical references (p...

Cold-air performance of compressor-drive turbine of Department of Energy upgraded automobile gas turbine engine /

Roelke, Richard J.
Haas, Jeffrey E.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.
Propulsion Laboratory (U.S.)
Lewis Research Center.

"October 1982"--Vol. II."Lewis Research Center.""June 1981"--Vol. I."AVRADCOM Research and Technolog...

Stability analysis for unloaded externally pressurized gas-lubricated bearings with journal rotation /

Fleming, David P.
Anderson, William J., 1922-
Cunningham, Robert E. (Robert Ernest)
United States. National Aeronautics and Space Administration.
Lewis Research Center.

Prepared at Lewis Research Center."December 1968"--Cover.Includes bibliographical references (p. 33)...

Performance study of rotating gas jet generator for strong traveling transverse acoustic modes /

Heidmann, Marcus F.
Lewis Research Center.
United States. National Aeronautics and Space Administration.

January 1968

Cover title."February 1968."Includes bibliographical references (p. 35).Mode of access: Internet

Reduction of apparent-power requirement of phase-controlled parasitically loaded turboalternator by multiple parasitic loads /

Gilbert, Leonard J.
Lewis Research Center.

Prepared at Lewis Research Center."February 1968"--Cover.Includes bibliographical references (p. 34)...

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...

Effect of pressure ratio and inlet pressure on performance of experimental gas turbine at inlet temperature of 800©� R /

Kohl, Robert C.
Larkin, Robert G., joint author.
United States. National Advisory Committee for Aeronautics. NACA research memorandum.
Lewis Flight Propulsion Laboratory.

On front cover: "November 2, 1948."Includes bibliographical references: p. 4.Mode of access: Interne...

Transient performance of a turboalternator gas-bearing system /

Wood, James C.
Asadourian, Armen S.
Curreri, Joseph S.
Lewis Research Center.
United States. National Aeronautics and Space Administration.

January 1970

Experimental operation of gas-bearing turboalternator for spacecraft power supplies.Includes bibliog...

Steady-state electrical performance of a 400-Hertz Brayton cycle turboalternator and controls /

Valgora, Martin E.
Perz, Dennis A.
United States. National Aeronautics and Space Administration.
Lewis Research Center.

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

Turbine performance in a gas-bearing Brayton cycle turboalternator /

Curreri, Joseph S.
Wood, James C.
Kruchowy, Roman.
Lewis Research Center.
United States. National Aeronautics and Space Administration.

January 1969

Turbine performance in gas-bearing Brayton cycle turboalternator.Includes bibliographical references...

Static parasitic speed controller for Brayton-cycle turboalternator /

Word, John L.
Ingle, Bill D.
Fischer, Raymond L. E.
Lewis Research Center.

Prepared at Lewis Research Center."September 1967"--Cover.Includes bibliographical references (p. 13...

Static sea-level performance of an axial-flow-compressor turbojet engine with an air-cooled turbine /

Cochran, Reeves P.
Dengler, Robert P.
Cochran, Reeves P.
Lewis Flight Propulsion Laboratory.
United States. National Adviosry Committee for Aeronautics. NACA research memorandum.
United States. National Advisory Committee for Aeronautics.

"Declassified February 10, 1959.""March 15, 1955."Cover title.Includes bibliographical references (p...

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...

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...

Steady-state performance of a modified Rankine cycle system using water /

Fenn, David B.
Gutierrez, Orlando A.
Coe, Harold H.
Lewis Research Center.

Prepared at Lewis Research Center."March 1966"--Cover.Includes bibliographical references (p. 18).Mo...

Experimental evaluation of volt-ampere loading and output distortion for a turboalternator with multiple load phase-controlled parasitic speed controller /

Perz, Dennis A.
Valgora, Martin E.
Lewis Research Center.

Prepared at Lewis Research Center."December 1969."Cover title.Includes bibliographical references (p...

Cold-air performance of compressor-drive turbine of Department of Energy upgraded automobile gas turbine engine /

Roelke, Richard J.
Haas, Jeffrey E.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.
Propulsion Laboratory (U.S.)
Lewis Research Center.

"October 1982"--Vol. II."Lewis Research Center.""June 1981"--Vol. I."AVRADCOM Research and Technolog...

Stability analysis for unloaded externally pressurized gas-lubricated bearings with journal rotation /

Fleming, David P.
Anderson, William J., 1922-
Cunningham, Robert E. (Robert Ernest)
United States. National Aeronautics and Space Administration.
Lewis Research Center.

Prepared at Lewis Research Center."December 1968"--Cover.Includes bibliographical references (p. 33)...

Performance study of rotating gas jet generator for strong traveling transverse acoustic modes /

Heidmann, Marcus F.
Lewis Research Center.
United States. National Aeronautics and Space Administration.

January 1968

Cover title."February 1968."Includes bibliographical references (p. 35).Mode of access: Internet

Reduction of apparent-power requirement of phase-controlled parasitically loaded turboalternator by multiple parasitic loads /

Gilbert, Leonard J.
Lewis Research Center.

Prepared at Lewis Research Center."February 1968"--Cover.Includes bibliographical references (p. 34)...

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...

Kohl, Robert C.
Larkin, Robert G., joint author.
United States. National Advisory Committee for Aeronautics. NACA research memorandum.
Lewis Flight Propulsion Laboratory.

On front cover: "November 2, 1948."Includes bibliographical references: p. 4.Mode of access: Interne...

Performance of a turboalternator gas-bearing system at steady-state conditions /

Abstract

Extracted data

Performance of a turboalternator gas-bearing system at steady-state conditions /

Abstract

Extracted data

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