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

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 modular combustor designed for a VTOL tip-turbine lift fan /

Marchionna, Nicholas R.
Lewis Research Center.
United States. National Aeronautics and Space Administration.

Prepared by Lewis Research Center."November 1971."--Cover.Major NASA subject terms: Combustion chamb...

Gust generator for a supersonic wind tunnel /

Sanders, Bobby W.
Webb, John A.
Bishop, Allan R.
Lewis Research Center.

January 1974

Prepared at Lewis Research Center.Cover title.Includes bibliographical references (p. 17).Mode of ac...

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...

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...

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...

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...

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

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...

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 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...

Drag and distribution measurements of single-element fuel injectors for supersonic combustors /

Povinelli, Louis A.
Lewis Research Center.

January 1974

Prepared at Lewis Research Center.Cover title.Includes bibliographical references (p. 22).Mode of ac...

Technique for predicting high-frequency stability characteristics of gaseous-propellant combustors /

Priem, Richard J.
Yang, Jefferson Y. S. (Jefferson Yuan Sheng), 1939-
Lewis Research Center.

January 1973

Prepared at Lewis Research Center.Cover title.Includes bibliographical references (p. 35).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...

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 modular combustor designed for a VTOL tip-turbine lift fan /

Marchionna, Nicholas R.
Lewis Research Center.
United States. National Aeronautics and Space Administration.

Prepared by Lewis Research Center."November 1971."--Cover.Major NASA subject terms: Combustion chamb...

Gust generator for a supersonic wind tunnel /

Sanders, Bobby W.
Webb, John A.
Bishop, Allan R.
Lewis Research Center.

January 1974

Prepared at Lewis Research Center.Cover title.Includes bibliographical references (p. 17).Mode of ac...

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...

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...

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...

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...

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

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...

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 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...

Drag and distribution measurements of single-element fuel injectors for supersonic combustors /

Povinelli, Louis A.
Lewis Research Center.

January 1974

Prepared at Lewis Research Center.Cover title.Includes bibliographical references (p. 22).Mode of ac...

Technique for predicting high-frequency stability characteristics of gaseous-propellant combustors /

Priem, Richard J.
Yang, Jefferson Y. S. (Jefferson Yuan Sheng), 1939-
Lewis Research Center.

January 1973

Prepared at Lewis Research Center.Cover title.Includes bibliographical references (p. 35).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...

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 modular combustor designed for a VTOL tip-turbine lift fan /

Marchionna, Nicholas R.
Lewis Research Center.
United States. National Aeronautics and Space Administration.

Prepared by Lewis Research Center."November 1971."--Cover.Major NASA subject terms: Combustion chamb...

Gust generator for a supersonic wind tunnel /

Sanders, Bobby W.
Webb, John A.
Bishop, Allan R.
Lewis Research Center.

January 1974

Prepared at Lewis Research Center.Cover title.Includes bibliographical references (p. 17).Mode of ac...

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

Abstract

Extracted data

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

Abstract

Extracted data

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