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

Film cooling in a combustor operating at fuel-rich exit conditions /

Tacina, Robert R.
Marek, Cecil J.
Lewis Research Center.

January 1974

Prepared at Lewis Research Center.Cover title.Includes bibliographical references (p. 19).Mode of ac...

Performance of a hydrogen burner to simulate air entering scramjet combustors /

Russin, William Roger.
Langley Research Center.

January 1974

Prepared at Langley Research Center.Cover title.Includes bibliographical references (p. 21).Mode of ...

Exploratory tests of two strut fuel injectors for supersonic combustion /

Anderson, Griffin Y.
Gooderum, Paul B.
Langley Research Center.

January 1974

Prepared at Langley Research Center.Cover title.Includes bibliographical references (p. 21).Mode of ...

Effect of design features on performance of a double-annular ram-induction combustor /

Schultz, Donald F.
Lewis Research Center.

January 1975

Prepared at Lewis Research Center.Cover title.Includes bibliographical references (p. 18-19).Mode of...

Exhaust emissions of a double annular combustor : parametric study /

Schultz, Donald F.
Lewis Research Center.

January 1974

Prepared at Lewis Research Center.Cover title.Includes bibliographical references (p. 19).Mode of ac...

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...

Idle efficiency and pollution results for two-row swirl-can combustors having 72 modules /

Biaglow, James A.
Trout, Arthur M.
Lewis Research Center.

January 1975

Prepared at Lewis Research Center.Cover title.Includes bibliographical references (p. 9).Mode of acc...

Measurements of liner cooling effectiveness within a full-scale double-annular ram-induction combustor /

Mularz, Edward J.
Schultz, Donald F.
U.S. Army Air Mobility Research and Development Laboratory.

January 1974

Prepared at Lewis Research Center and the U.S. Army Air Mobility R&D Laboratory.Cover title.Includes...

Effect of diffuser bleed on performance of an annular swirl can combustor /

Juhasz, Albert J.
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 /

Zettle, Eugene V.
Mark, Herman, joint author.
United States. National Advisory Committee for Aeronautics. NACA research memorandum.
Lewis Flight Propulsion Laboratory.

On front cover: "August 3, 1950."Includes bibliographical references: p. 12.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...

Effect of oxygen addition on altitude blowout and relight of an experimental combustor segment /

Norgren, Carl T.
Ingebo, Robert D.
Lewis Research Center.

January 1974

Prepared at Lewis Research Center.Cover title.Includes bibliographical references (p. 7).Mode of acc...

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)....

Use of an air-assist fuel nozzle to reduce exhaust emissions from a gas-turbine combustor at simulated idle conditions /

Briehl, Daniel.
Papathakos, Leonidas.
Lewis Research Center.
United States. National Aeronautics and Space Administration.

January 1971

Use of air-assist fuel nozzle to reduce exhaust emissions from gas turbine combustor at simulated id...

Some aspects of FLOX-methane rocket engine throttling /

Sokolowski, D. E. (Daniel E.)
Seigwarth, Edwin J.
Hannum, Ned P.
Lewis Research Center.

January 1974

Prepared at Lewis Research Center.Cover title.Includes bibliographical references (p. 15).Mode of ac...

Film cooling in a combustor operating at fuel-rich exit conditions /

Tacina, Robert R.
Marek, Cecil J.
Lewis Research Center.

January 1974

Prepared at Lewis Research Center.Cover title.Includes bibliographical references (p. 19).Mode of ac...

Performance of a hydrogen burner to simulate air entering scramjet combustors /

Russin, William Roger.
Langley Research Center.

January 1974

Prepared at Langley Research Center.Cover title.Includes bibliographical references (p. 21).Mode of ...

Exploratory tests of two strut fuel injectors for supersonic combustion /

Anderson, Griffin Y.
Gooderum, Paul B.
Langley Research Center.

January 1974

Prepared at Langley Research Center.Cover title.Includes bibliographical references (p. 21).Mode of ...

Effect of design features on performance of a double-annular ram-induction combustor /

Schultz, Donald F.
Lewis Research Center.

January 1975

Prepared at Lewis Research Center.Cover title.Includes bibliographical references (p. 18-19).Mode of...

Exhaust emissions of a double annular combustor : parametric study /

Schultz, Donald F.
Lewis Research Center.

January 1974

Prepared at Lewis Research Center.Cover title.Includes bibliographical references (p. 19).Mode of ac...

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...

Idle efficiency and pollution results for two-row swirl-can combustors having 72 modules /

Biaglow, James A.
Trout, Arthur M.
Lewis Research Center.

January 1975

Prepared at Lewis Research Center.Cover title.Includes bibliographical references (p. 9).Mode of acc...

Measurements of liner cooling effectiveness within a full-scale double-annular ram-induction combustor /

Mularz, Edward J.
Schultz, Donald F.
U.S. Army Air Mobility Research and Development Laboratory.

January 1974

Prepared at Lewis Research Center and the U.S. Army Air Mobility R&D Laboratory.Cover title.Includes...

Effect of diffuser bleed on performance of an annular swirl can combustor /

Juhasz, Albert J.
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 /

Zettle, Eugene V.
Mark, Herman, joint author.
United States. National Advisory Committee for Aeronautics. NACA research memorandum.
Lewis Flight Propulsion Laboratory.

On front cover: "August 3, 1950."Includes bibliographical references: p. 12.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...

Effect of oxygen addition on altitude blowout and relight of an experimental combustor segment /

Norgren, Carl T.
Ingebo, Robert D.
Lewis Research Center.

January 1974

Prepared at Lewis Research Center.Cover title.Includes bibliographical references (p. 7).Mode of acc...

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)....

Use of an air-assist fuel nozzle to reduce exhaust emissions from a gas-turbine combustor at simulated idle conditions /

Briehl, Daniel.
Papathakos, Leonidas.
Lewis Research Center.
United States. National Aeronautics and Space Administration.

January 1971

Use of air-assist fuel nozzle to reduce exhaust emissions from gas turbine combustor at simulated id...

Some aspects of FLOX-methane rocket engine throttling /

Sokolowski, D. E. (Daniel E.)
Seigwarth, Edwin J.
Hannum, Ned P.
Lewis Research Center.

January 1974

Prepared at Lewis Research Center.Cover title.Includes bibliographical references (p. 15).Mode of ac...

Film cooling in a combustor operating at fuel-rich exit conditions /

Tacina, Robert R.
Marek, Cecil J.
Lewis Research Center.

January 1974

Prepared at Lewis Research Center.Cover title.Includes bibliographical references (p. 19).Mode of ac...

Performance of a hydrogen burner to simulate air entering scramjet combustors /

Russin, William Roger.
Langley Research Center.

January 1974

Prepared at Langley Research Center.Cover title.Includes bibliographical references (p. 21).Mode of ...

Exploratory tests of two strut fuel injectors for supersonic combustion /

Anderson, Griffin Y.
Gooderum, Paul B.
Langley Research Center.

January 1974

Prepared at Langley Research Center.Cover title.Includes bibliographical references (p. 21).Mode of ...

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

Abstract

Extracted data

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

Abstract

Extracted data

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