Simulated altitude performance of two annular combustors with continuous axial openings for admission of primary air /

Low-pressure performance of experimental prevaporizing tubular combustor using approximately stoichiometric admission of fuel-air mixture into the primary zone /

Hibbard, Robert R.
Scull, Wilfred E., joint author.
Metzler, Allen J., joint author.
United States. National Advisory Committee for Aeronautics. NACA research memorandum.
Lewis Flight Propulsion Laboratory.

On front cover: "August 19, 1954."Title from cover.Includes bibliographical references: p. 14-15.Mod...

Investigation of the I-40 Jet-Propulsion Engine in the Cleveland Altitude Wind Tunnel

Krebs, Richard P.
Foshag, Frederick C., joint author.
United States. National Advisory Committee for Aeronautics. NACA research memorandum.
Flight Propulsion Research Laboratory.

On front cover: "August 26, 1948."Includes bibliographical references: p. 12-13.Mode of access: Inte...

Variable combustor geometry for improving the altitude relight capability of a double annular combustor /

Schultz, Donald F.
Lewis Research Center.

January 1974

Prepared at Lewis Research Center.Cover title.Includes bibliographical references (p. 12).Mode of ac...

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

An experimental study of five annular air inlet configurations at subsonic and transonic speeds /

Bryan, Carroll R.
Fleming, Frank F.
Milillo, Jospeh R.
Pendley, Robert E.
Langley Aeronautical Laboratory.
United States. National Adviosry Committee for Aeronautics. NACA research memorandum.

January 1953

"August 19, 1953."Includes bibliographical references (p. 22-23).Mode of access: Internet

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

Modifications that improve performance of a double annular combustor at simulated engine idle conditions /

Schultz, Donald F.
Lewis Research Center.

January 1974

Prepared at Lewis Research Center.Cover title.Includes bibliographical references (p. 18).Mode of ac...

Altitude-wind-tunnel investigation of Westinghouse 19B-2 19B-8, and 19XB-1 jet-propulsion engines

Boyd, Bemrose
United States. National Advisory Committee for Aeronautics. NACA research memorandum.
Lewis Flight Propulsion Laboratory.

On front cover: "November 26, 1948."Includes bibliographical references: p. 20.Mode of access: Inter...

Altitude-wind-tunnel investigation of Westinghouse 19B-2 19B-8, and 19XB-1 jet-propulsion engines

Fleming, William A.
Dietz, Robert O. Jr. joint author.
United States. National Advisory Committee for Aeronautics. NACA research memorandum.
Lewis Flight Propulsion Laboratory.

On front cover: "November 26, 1948."Includes bibliographical references: p. 17.Mode of access: Inter...

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

Cook, William P.
Koch, Richard G., joint author.
United States. National Advisory Committee for Aeronautics. NACA research memorandum.
Lewis Flight Propulsion Laboratory.

On front cover: "February 28, 1950."Includes bibliographical references (p. 11).Mode of access: Inte...

Experimental investigation of two-stage air-cooled turbine suitable for flight at Mach 2.5 /

Schum, Harold J.
Nunamaker, Robert R.
Petrash, Donald A.
Lewis Research Center.
United States. National Aeronautics and Space Administration.

January 1959

"November 1959."Cover title.Includes bibliographical references (p. 27).Mode of access: Internet

Altitude-wind-tunnel investigation of Westinghouse 19B-2 19B-8, and 19XB-1 jet-propulsion engines

Dietz, Robert O.
Kuenzig, John K., joint author.
United States. National Advisory Committee for Aeronautics. NACA research memorandum.
Lewis Flight Propulsion Laboratory.

On front cover: "November 26, 1948."Includes bibliographical references: p. 16.Mode of access: Inter...

Starting of rocket engine at conditions of simulated altitude using crude monoethylaniline and other fuels with mixed acid /

Morrell, Gerald joint author.
Humphrey, Jack C., joint author.
Sloop, John L., joint author.
Ladanyi, Dezso J., joint author.
United States. National Advisory Committee for Aeronautics. NACA research memorandum.
Lewis Flight Propulsion Laboratory.

On front cover: "July 19, 1950."Includes bibliographical references: p. 16.Mode of access: Internet

Investigation of the I-40 Jet-Propulsion Engine in the Cleveland Altitude Wind Tunnel

Golladay, Richard L.
Gendler, Stanley L., joint author.
United States. National Advisory Committee for Aeronautics. NACA research memorandum.
Flight Propulsion Research Laboratory.

On front cover: "August 25, 1948."Includes bibliographical references: p. 26-27.Mode of access: Inte...

Altitude-wind-tunnel investigation of Westinghouse 19B-2 19B-8, and 19XB-1 jet-propulsion engines

Krebs, Richard P.
Suozzi, Frank L., joint author.
United States. National Advisory Committee for Aeronautics. NACA research memorandum.
Lewis Flight Propulsion Laboratory.

On front cover: "November 24, 1948."Includes bibliographical references: p. 11.Mode of access: Inter...

Low-pressure performance of experimental prevaporizing tubular combustor using approximately stoichiometric admission of fuel-air mixture into the primary zone /

Hibbard, Robert R.
Scull, Wilfred E., joint author.
Metzler, Allen J., joint author.
United States. National Advisory Committee for Aeronautics. NACA research memorandum.
Lewis Flight Propulsion Laboratory.

On front cover: "August 19, 1954."Title from cover.Includes bibliographical references: p. 14-15.Mod...

Investigation of the I-40 Jet-Propulsion Engine in the Cleveland Altitude Wind Tunnel

Krebs, Richard P.
Foshag, Frederick C., joint author.
United States. National Advisory Committee for Aeronautics. NACA research memorandum.
Flight Propulsion Research Laboratory.

On front cover: "August 26, 1948."Includes bibliographical references: p. 12-13.Mode of access: Inte...

Variable combustor geometry for improving the altitude relight capability of a double annular combustor /

Schultz, Donald F.
Lewis Research Center.

January 1974

Prepared at Lewis Research Center.Cover title.Includes bibliographical references (p. 12).Mode of ac...

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

An experimental study of five annular air inlet configurations at subsonic and transonic speeds /

Bryan, Carroll R.
Fleming, Frank F.
Milillo, Jospeh R.
Pendley, Robert E.
Langley Aeronautical Laboratory.
United States. National Adviosry Committee for Aeronautics. NACA research memorandum.

January 1953

"August 19, 1953."Includes bibliographical references (p. 22-23).Mode of access: Internet

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

Modifications that improve performance of a double annular combustor at simulated engine idle conditions /

Schultz, Donald F.
Lewis Research Center.

January 1974

Prepared at Lewis Research Center.Cover title.Includes bibliographical references (p. 18).Mode of ac...

Altitude-wind-tunnel investigation of Westinghouse 19B-2 19B-8, and 19XB-1 jet-propulsion engines

Boyd, Bemrose
United States. National Advisory Committee for Aeronautics. NACA research memorandum.
Lewis Flight Propulsion Laboratory.

On front cover: "November 26, 1948."Includes bibliographical references: p. 20.Mode of access: Inter...

Altitude-wind-tunnel investigation of Westinghouse 19B-2 19B-8, and 19XB-1 jet-propulsion engines

Fleming, William A.
Dietz, Robert O. Jr. joint author.
United States. National Advisory Committee for Aeronautics. NACA research memorandum.
Lewis Flight Propulsion Laboratory.

On front cover: "November 26, 1948."Includes bibliographical references: p. 17.Mode of access: Inter...

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

Cook, William P.
Koch, Richard G., joint author.
United States. National Advisory Committee for Aeronautics. NACA research memorandum.
Lewis Flight Propulsion Laboratory.

On front cover: "February 28, 1950."Includes bibliographical references (p. 11).Mode of access: Inte...

Experimental investigation of two-stage air-cooled turbine suitable for flight at Mach 2.5 /

Schum, Harold J.
Nunamaker, Robert R.
Petrash, Donald A.
Lewis Research Center.
United States. National Aeronautics and Space Administration.

January 1959

"November 1959."Cover title.Includes bibliographical references (p. 27).Mode of access: Internet

Altitude-wind-tunnel investigation of Westinghouse 19B-2 19B-8, and 19XB-1 jet-propulsion engines

Dietz, Robert O.
Kuenzig, John K., joint author.
United States. National Advisory Committee for Aeronautics. NACA research memorandum.
Lewis Flight Propulsion Laboratory.

On front cover: "November 26, 1948."Includes bibliographical references: p. 16.Mode of access: Inter...

Starting of rocket engine at conditions of simulated altitude using crude monoethylaniline and other fuels with mixed acid /

Morrell, Gerald joint author.
Humphrey, Jack C., joint author.
Sloop, John L., joint author.
Ladanyi, Dezso J., joint author.
United States. National Advisory Committee for Aeronautics. NACA research memorandum.
Lewis Flight Propulsion Laboratory.

On front cover: "July 19, 1950."Includes bibliographical references: p. 16.Mode of access: Internet

Investigation of the I-40 Jet-Propulsion Engine in the Cleveland Altitude Wind Tunnel

Golladay, Richard L.
Gendler, Stanley L., joint author.
United States. National Advisory Committee for Aeronautics. NACA research memorandum.
Flight Propulsion Research Laboratory.

On front cover: "August 25, 1948."Includes bibliographical references: p. 26-27.Mode of access: Inte...

Altitude-wind-tunnel investigation of Westinghouse 19B-2 19B-8, and 19XB-1 jet-propulsion engines

Krebs, Richard P.
Suozzi, Frank L., joint author.
United States. National Advisory Committee for Aeronautics. NACA research memorandum.
Lewis Flight Propulsion Laboratory.

On front cover: "November 24, 1948."Includes bibliographical references: p. 11.Mode of access: Inter...

Low-pressure performance of experimental prevaporizing tubular combustor using approximately stoichiometric admission of fuel-air mixture into the primary zone /

Hibbard, Robert R.
Scull, Wilfred E., joint author.
Metzler, Allen J., joint author.
United States. National Advisory Committee for Aeronautics. NACA research memorandum.
Lewis Flight Propulsion Laboratory.

On front cover: "August 19, 1954."Title from cover.Includes bibliographical references: p. 14-15.Mod...

Investigation of the I-40 Jet-Propulsion Engine in the Cleveland Altitude Wind Tunnel

Krebs, Richard P.
Foshag, Frederick C., joint author.
United States. National Advisory Committee for Aeronautics. NACA research memorandum.
Flight Propulsion Research Laboratory.

On front cover: "August 26, 1948."Includes bibliographical references: p. 12-13.Mode of access: Inte...

Variable combustor geometry for improving the altitude relight capability of a double annular combustor /

Schultz, Donald F.
Lewis Research Center.

January 1974

Prepared at Lewis Research Center.Cover title.Includes bibliographical references (p. 12).Mode of ac...

Simulated altitude performance of two annular combustors with continuous axial openings for admission of primary air /

Abstract

Extracted data

Simulated altitude performance of two annular combustors with continuous axial openings for admission of primary air /

Abstract

Extracted data

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