Performance investigation of can-type combustor from British turbojet engine and comparison of this combustor with can-type combustor from U.S. turbojet engine /

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

Experimental investigation of air-cooled turbine blades in turbojet engine

Hickel, Robert O.
Smith, Gordon T., joint author.
United States. National Advisory Committee for Aeronautics. NACA research memorandum.
Lewis Flight Propulsion Laboratory.

On front cover: "December 11, 1950."Title from cover.Includes bibliographical references: p. 15.Mode...

Photographic studies of preignition environment and flame initiation in turbojet-engine combustors /

Straight, David M.
Gernon, J. Dean, joint author.
United States. National Advisory Committee for Aeronautics. NACA research memorandum.
Lewis Flight Propulsion Laboratory.

On front cover: "February 6, 1953."Title from cover.Includes bibliographical references: p. 15-16.Mo...

Performance comparisons of JFC-2 and MIL-F-5624A (JP-3) fuels in tubular and annular combustors /

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

January 1952

"January 23, 1952."Includes bibliographical references (p. 6).Mode of access: Internet

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...

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 experimental channeled-wall annular turbojet combustor at conditions simulating high-altitude supersonic flight.

Zettle, Eugene V.
Friedman, Robert, 1929-
Lewis Flight Propulsion Laboratory.
United States. National Adviosry Committee for Aeronautics. NACA research memorandum.
United States. National Advisory Committee for Aeronautics.

January 1955

"March 15, 1955."Includes bibliographical references (p. 7).Mode of access: Internet

Preliminary investigation of effects of combustion in ram jet on performance of supersonic diffusers.

Schroeder, Albert H.
Connors, James F., joint author.
United States. National Advisory Committee for Aeronautics. NACA research memorandum.
Lewis Flight Propulsion Laboratory.

On front cover: "December 22, 1948."Title from cover.Includes bibliographical references (p. 6).Mode...

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

Low-pressure performance of different diameter experimental combustor liners /

Dittrich, Ralph T.
Lewis Flight Propulsion Laboratory.
United States. National Adviosry Committee for Aeronautics. NACA research memorandum.

January 1954

"February 19, 1954."Cover title.Includes bibliographical references (p. 14-15).Mode of access: Inter...

Performance of J33 turbojet engine with shaft-power extraction

Nettles, J. C.
Easterly, J. R., joint author.
United States. National Advisory Committee for Aeronautics. NACA research memorandum.
Flight Propulsion Research Laboratory.

On front cover: "May 28, 1948."Includes bibliographical references: p. 11.Mode of access: Internet

Performance of swirl-can turbojet combustors at simulated supersonic combustor-inlet conditions /

Butze, Helmut F.
Lewis Research Center.
United States. National Aeronautics and Space Administration.

January 1969

Prepared at Lewis Research Center.N69-16154.Cover title.Includes bibliographical references (p. 25)....

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 acceleration characteristics of a single-spool turbojet engine /

Oppenheimer, Frank L.
Pack, George J., joint author.
United States. National Advisory Committee for Aeronautics. NACA research memorandum.
Lewis Flight Propulsion Laboratory.

On front cover: "October 26, 1953."Title from cover.Includes bibliographical references: p. 13.Mode ...

Comparison of the performance of a helicopter-type ram-jet engine under various centrifugal loadings /

Radin, Edward J.
Carpenter, Paul J.
Langley Aeronautical Laboratory.
United States. National Adviosry Committee for Aeronautics. NACA research memorandum.

January 1953

"October 7, 1953."Includes bibliographical references (p. 9).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

Experimental investigation of air-cooled turbine blades in turbojet engine

Hickel, Robert O.
Smith, Gordon T., joint author.
United States. National Advisory Committee for Aeronautics. NACA research memorandum.
Lewis Flight Propulsion Laboratory.

On front cover: "December 11, 1950."Title from cover.Includes bibliographical references: p. 15.Mode...

Photographic studies of preignition environment and flame initiation in turbojet-engine combustors /

Straight, David M.
Gernon, J. Dean, joint author.
United States. National Advisory Committee for Aeronautics. NACA research memorandum.
Lewis Flight Propulsion Laboratory.

On front cover: "February 6, 1953."Title from cover.Includes bibliographical references: p. 15-16.Mo...

Performance comparisons of JFC-2 and MIL-F-5624A (JP-3) fuels in tubular and annular combustors /

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

January 1952

"January 23, 1952."Includes bibliographical references (p. 6).Mode of access: Internet

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...

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 experimental channeled-wall annular turbojet combustor at conditions simulating high-altitude supersonic flight.

Zettle, Eugene V.
Friedman, Robert, 1929-
Lewis Flight Propulsion Laboratory.
United States. National Adviosry Committee for Aeronautics. NACA research memorandum.
United States. National Advisory Committee for Aeronautics.

January 1955

"March 15, 1955."Includes bibliographical references (p. 7).Mode of access: Internet

Preliminary investigation of effects of combustion in ram jet on performance of supersonic diffusers.

Schroeder, Albert H.
Connors, James F., joint author.
United States. National Advisory Committee for Aeronautics. NACA research memorandum.
Lewis Flight Propulsion Laboratory.

On front cover: "December 22, 1948."Title from cover.Includes bibliographical references (p. 6).Mode...

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

Low-pressure performance of different diameter experimental combustor liners /

Dittrich, Ralph T.
Lewis Flight Propulsion Laboratory.
United States. National Adviosry Committee for Aeronautics. NACA research memorandum.

January 1954

"February 19, 1954."Cover title.Includes bibliographical references (p. 14-15).Mode of access: Inter...

Performance of J33 turbojet engine with shaft-power extraction

Nettles, J. C.
Easterly, J. R., joint author.
United States. National Advisory Committee for Aeronautics. NACA research memorandum.
Flight Propulsion Research Laboratory.

On front cover: "May 28, 1948."Includes bibliographical references: p. 11.Mode of access: Internet

Performance of swirl-can turbojet combustors at simulated supersonic combustor-inlet conditions /

Butze, Helmut F.
Lewis Research Center.
United States. National Aeronautics and Space Administration.

January 1969

Prepared at Lewis Research Center.N69-16154.Cover title.Includes bibliographical references (p. 25)....

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 acceleration characteristics of a single-spool turbojet engine /

Oppenheimer, Frank L.
Pack, George J., joint author.
United States. National Advisory Committee for Aeronautics. NACA research memorandum.
Lewis Flight Propulsion Laboratory.

On front cover: "October 26, 1953."Title from cover.Includes bibliographical references: p. 13.Mode ...

Comparison of the performance of a helicopter-type ram-jet engine under various centrifugal loadings /

Radin, Edward J.
Carpenter, Paul J.
Langley Aeronautical Laboratory.
United States. National Adviosry Committee for Aeronautics. NACA research memorandum.

January 1953

"October 7, 1953."Includes bibliographical references (p. 9).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

Experimental investigation of air-cooled turbine blades in turbojet engine

Hickel, Robert O.
Smith, Gordon T., joint author.
United States. National Advisory Committee for Aeronautics. NACA research memorandum.
Lewis Flight Propulsion Laboratory.

On front cover: "December 11, 1950."Title from cover.Includes bibliographical references: p. 15.Mode...

Photographic studies of preignition environment and flame initiation in turbojet-engine combustors /

Straight, David M.
Gernon, J. Dean, joint author.
United States. National Advisory Committee for Aeronautics. NACA research memorandum.
Lewis Flight Propulsion Laboratory.

On front cover: "February 6, 1953."Title from cover.Includes bibliographical references: p. 15-16.Mo...

Performance investigation of can-type combustor from British turbojet engine and comparison of this combustor with can-type combustor from U.S. turbojet engine /

Abstract

Extracted data

Performance investigation of can-type combustor from British turbojet engine and comparison of this combustor with can-type combustor from U.S. turbojet engine /

Abstract

Extracted data

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