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

Investigations of air-cooled turbine rotors for turbojet engines

Nachtigall, Alfred J.
Ziemer, Robert R., joint author.
Zalabak, Charles F., joint author.
United States. National Advisory Committee for Aeronautics. NACA research memorandum.
Lewis Flight Propulsion Laboratory.

On front cover: "May 21, 1952."Title from cover.Includes bibliographical references: p. 22.Mode of a...

Static investigation of several jet deflectors for longitudinal control of an aircraft /

Valerino, Alfred S.
United States. National Advisory Committee for Aeronautics. NACA research memorandum.
Lewis Flight Propulsion Laboratory.

On front cover: "June 7, 1955."Title from cover.Includes bibliographical references: p. 9.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...

Transient and steady-state performance of a single turbojet combustor with four different fuel nozzles /

McCafferty, Richard J.
Donlon, Richard H.
Lewis Flight Propulsion Laboratory.
United States. National Adviosry Committee for Aeronautics. NACA research memorandum.
United States. National Advisory Committee for Aeronautics.

January 1955

"Declassified October 31, 1958.""October 21, 1955."Cover title.Includes bibliographical references (...

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

Evaluation of a compressor bleed system for rim cooling the turbine wheel of a turbojet engine /

Morse, C. R.
Kemp, R. H.
United States. National Advisory Committee for Aeronautics.

"Declassified February 10, 1959.""March 22, 1954."Cover title.Includes bibliographical references (p...

Investigation of the performance of a turbojet engine with variable-position compressor inlet guide vanes /

Budinger, Ray E.
Kaufman, Harold R.
Lewis Flight Propulsion Laboratory.
United States. National Adviosry Committee for Aeronautics. NACA research memorandum.

January 1955

"October 4, 1955."Includes bibliographical references (p. 20).Mode of access: Internet

Dynamics of a supersonic inlet with adjustable bypass in combination with a J34 turbojet engine /

Wilcox, Fred.
Whalen, Paul.
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 23, 1956."Cover title.Includes bibliographical references (p...

Efficiency of radial-flow turbine of turbo engineering corporation TT13-18 turbosupercharger/

Coulter, Earl E.
Galloway, William R., joint author.
United States. National Advisory Committee for Aeronautics. NACA research memorandum.
Flight Propulsion Research Laboratory.

On front cover: "December 8, 1947."At head of title: "for the Bureau of Aeronautics, Navy Department...

Altitude-wind-tunnel investigation of a 4000-pound-thrust axial-flow turbojet engine

Fleming, William A.
United States. National Advisory Committee for Aeronautics. NACA research memorandum.
Flight Propulsion Research Laboratory.

On front cover: "August 3, 1948."Includes bibliographical references: p. 17.Mode of access: Internet

Experimental investigation of a transonic axial-flow-compressor rotor with double-circular-arc airfoil blade sections.

Lewis, George W., Jr.
Serovy, G. K. (George K.)
Schwenk, Francis C.
Lewis Flight Propulsion Laboratory.
United States. National Adviosry Committee for Aeronautics. NACA research memorandum.

January 1954

"Declassified October 31, 1958.""April 5, 1954."Cover title.Includes bibliographical references (p. ...

Effect of a reduction in stator solidity on performance of a transonic turbine /

Miser, James W.
Wong, Robert Y.
Stewart, Warner L.
Lewis Flight Propulsion Laboratory.
United States. National Adviosry Committee for Aeronautics. NACA research memorandum.
United States. National Advisory Committee for Aeronautics.

"Declassified December 3, 1958.""March 23, 1956."Cover title.Includes bibliographical references (p....

Turbojet combustor performance with injection of hydrogen peroxide for thrust augmentation /

Metzler, Allen J.
Grobman, Jack S.
Lewis Flight Propulsion Laboratory.
United States. National Adviosry Committee for Aeronautics. NACA research memorandum.
United States. National Advisory Committee for Aeronautics.

January 1956

"Declassified October 31, 1958.""April 17, 1956."Cover title.Includes bibliographical references (p....

Investigation of an impulse axial-flow compressor rotor over a range of blade angles /

Schulze, Wallace M.
Westphal, Willard R.
Erwin, John R.
Langley Aeronautical Laboratory.
United States. National Adviosry Committee for Aeronautics. NACA research memorandum.

January 1950

"August 29, 1950."Cover title.Includes bibliographical references (p. 16).Mode of access: Internet

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

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

Turboalternator gas-bearing system performance at steady state conditions.Prepared at Lewis Research...

Investigations of air-cooled turbine rotors for turbojet engines

Nachtigall, Alfred J.
Ziemer, Robert R., joint author.
Zalabak, Charles F., joint author.
United States. National Advisory Committee for Aeronautics. NACA research memorandum.
Lewis Flight Propulsion Laboratory.

On front cover: "May 21, 1952."Title from cover.Includes bibliographical references: p. 22.Mode of a...

Static investigation of several jet deflectors for longitudinal control of an aircraft /

Valerino, Alfred S.
United States. National Advisory Committee for Aeronautics. NACA research memorandum.
Lewis Flight Propulsion Laboratory.

On front cover: "June 7, 1955."Title from cover.Includes bibliographical references: p. 9.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...

Transient and steady-state performance of a single turbojet combustor with four different fuel nozzles /

McCafferty, Richard J.
Donlon, Richard H.
Lewis Flight Propulsion Laboratory.
United States. National Adviosry Committee for Aeronautics. NACA research memorandum.
United States. National Advisory Committee for Aeronautics.

January 1955

"Declassified October 31, 1958.""October 21, 1955."Cover title.Includes bibliographical references (...

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

Evaluation of a compressor bleed system for rim cooling the turbine wheel of a turbojet engine /

Morse, C. R.
Kemp, R. H.
United States. National Advisory Committee for Aeronautics.

"Declassified February 10, 1959.""March 22, 1954."Cover title.Includes bibliographical references (p...

Investigation of the performance of a turbojet engine with variable-position compressor inlet guide vanes /

Budinger, Ray E.
Kaufman, Harold R.
Lewis Flight Propulsion Laboratory.
United States. National Adviosry Committee for Aeronautics. NACA research memorandum.

January 1955

"October 4, 1955."Includes bibliographical references (p. 20).Mode of access: Internet

Dynamics of a supersonic inlet with adjustable bypass in combination with a J34 turbojet engine /

Wilcox, Fred.
Whalen, Paul.
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 23, 1956."Cover title.Includes bibliographical references (p...

Efficiency of radial-flow turbine of turbo engineering corporation TT13-18 turbosupercharger/

Coulter, Earl E.
Galloway, William R., joint author.
United States. National Advisory Committee for Aeronautics. NACA research memorandum.
Flight Propulsion Research Laboratory.

On front cover: "December 8, 1947."At head of title: "for the Bureau of Aeronautics, Navy Department...

Altitude-wind-tunnel investigation of a 4000-pound-thrust axial-flow turbojet engine

Fleming, William A.
United States. National Advisory Committee for Aeronautics. NACA research memorandum.
Flight Propulsion Research Laboratory.

On front cover: "August 3, 1948."Includes bibliographical references: p. 17.Mode of access: Internet

Experimental investigation of a transonic axial-flow-compressor rotor with double-circular-arc airfoil blade sections.

Lewis, George W., Jr.
Serovy, G. K. (George K.)
Schwenk, Francis C.
Lewis Flight Propulsion Laboratory.
United States. National Adviosry Committee for Aeronautics. NACA research memorandum.

January 1954

"Declassified October 31, 1958.""April 5, 1954."Cover title.Includes bibliographical references (p. ...

Effect of a reduction in stator solidity on performance of a transonic turbine /

Miser, James W.
Wong, Robert Y.
Stewart, Warner L.
Lewis Flight Propulsion Laboratory.
United States. National Adviosry Committee for Aeronautics. NACA research memorandum.
United States. National Advisory Committee for Aeronautics.

"Declassified December 3, 1958.""March 23, 1956."Cover title.Includes bibliographical references (p....

Turbojet combustor performance with injection of hydrogen peroxide for thrust augmentation /

Metzler, Allen J.
Grobman, Jack S.
Lewis Flight Propulsion Laboratory.
United States. National Adviosry Committee for Aeronautics. NACA research memorandum.
United States. National Advisory Committee for Aeronautics.

January 1956

"Declassified October 31, 1958.""April 17, 1956."Cover title.Includes bibliographical references (p....

Investigation of an impulse axial-flow compressor rotor over a range of blade angles /

Schulze, Wallace M.
Westphal, Willard R.
Erwin, John R.
Langley Aeronautical Laboratory.
United States. National Adviosry Committee for Aeronautics. NACA research memorandum.

January 1950

"August 29, 1950."Cover title.Includes bibliographical references (p. 16).Mode of access: Internet

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

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

Turboalternator gas-bearing system performance at steady state conditions.Prepared at Lewis Research...

Investigations of air-cooled turbine rotors for turbojet engines

Nachtigall, Alfred J.
Ziemer, Robert R., joint author.
Zalabak, Charles F., joint author.
United States. National Advisory Committee for Aeronautics. NACA research memorandum.
Lewis Flight Propulsion Laboratory.

On front cover: "May 21, 1952."Title from cover.Includes bibliographical references: p. 22.Mode of a...

Static investigation of several jet deflectors for longitudinal control of an aircraft /

Valerino, Alfred S.
United States. National Advisory Committee for Aeronautics. NACA research memorandum.
Lewis Flight Propulsion Laboratory.

On front cover: "June 7, 1955."Title from cover.Includes bibliographical references: p. 9.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...

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

Abstract

Extracted data

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

Abstract

Extracted data

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