Effect of wall edge suction on the performance of a short annular dump diffuser with exit passage flow resistance /

Effect on fan flow characteristics of length and axial location of a cascade thrust reverser /

Dietrich, Donald A. (Donald Arthur), 1943-
Kelm, Gary G.
Crooker, Andrew J. (Andrew Jackson), 1939-
Lewis Research Center.

January 1975

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

The effect of the inlet mach number and inlet-boundary-layer thickness on the performance of a 23©� conical-diffuser-tail-pipe combination /

Persh, Jerome.
Langley Aeronautical Laboratory.
United States. National Adviosry Committee for Aeronautics. NACA research memorandum.

January 1950

"March 21, 1950."Includes bibliographical references (p. 21).Mode of access: Internet

Experimental and analytical study of a conically diffused flow with a nearly separated boundary layer /

Boldman, Donald R.
Neumann, Harvey E.
Lewis Research Center.

January 1973

Prepared at Lewis Research Center.Cover title.Includes bibliographical references (p. 38-39).Mode of...

Effect of wall suction on performance of a short annular diffuser at inlet Mach numbers up to 0.5 /

Juhasz, Albert J.
Lewis Research Center.

January 1975

Prepared at Lewis Research Center.Cover title.Bibliography: p. 12-13.Mode of access: Internet

Design and experimental performance of short curved wall diffusers with axial symmetry utilizing slot suction /

Yang, Tah-teh.
Nelson, Carl D.
Hudson, William G.
Lewis Research Center.
Clemson University.

January 1973

"Prepared by Clemson University ... for Lewis Research Center."Cover title.Bibliography: p. 40.Mode ...

Effect of wall edge suction on the performance of a short annular dump diffuser with exit passage flow resistance

Juhasz, A. J.

April 1975

The effect of wall edge suction on the performance of a short annular dump diffuser having a perfora...

Performance of high-area-ratio annular dump diffuser using suction-stabilized-vortex flow control /

Juhasz, Albert J.
Smith, John M., joint author.
United States. National Aeronautics and Space Administration.

January 1977

Issued May 1977.Includes bibliographical references (p. 19).Mode of access: Internet

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...

Effects of suction boundary-layer control on the performance of a short annular diffuser with an upstream terminal normal shock /

Shoemaker, Charles J.
Henry, John R.
United States. National Aeronautics and Space Administration.

Cover title."April 1962."Aerodynamics, aircraft; Propulsion system elements; Propulsion systems, air...

Effect of inducer inlet and diffuser throat areas on performance of a low pressure ratio sweptback centrifugal compressor /

Klassen, Hugh A.
Lewis Research Center.

January 1975

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

Reduction of wind-tunnel wall interference by controlled wall flow /

Bernstein, Samuel.
Joppa, Robert G. (Robert Glenn)
University of Washington. Dept. of Aeronautics and Astronautics.
United States. National Aeronautics and Space Administration.

January 1976

Cover title.Includes bibliographical references (p. 47-49).Mode of access: Internet

Flow and wall-temperature sensitivity in parallel passages for large inlet to exit density ratios in subsonic flow /

Reshotko, Meyer.
Lewis Research Center.
United States. National Aeronautics and Space Administration.

January 1968

Cover title."July 1968."Includes bibliographical references (p. 28).Mode of access: Internet

An experimental study of near wall flow parameters in the blade end-wall corner region /

Bhargava, Rakesh K.
Raj, Rishi S.
Lewis Research Center.

January 1989

"Prepared for Lewis Research Center under Grant NAG3-122."Bibliography: p. 282-297.Mode of access: I...

An investigation of the flow characteristics in the blade endwall corner region /

Hazarika, Birinchi K.
Raj, Rishi.
Lewis Research Center.

January 1987

"July 1987"--Cover."Prepared for Lewis Research Center under Contract NAS3-122."Includes bibliograph...

Transonic off-design drag and performance of three mixed-compression axisymmetric inlets /

Woollett, Richard R.
Choby, David A.
Meleason, Edward T.
Lewis Research Center.

January 1975

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

Effect on fan flow characteristics of length and axial location of a cascade thrust reverser /

Dietrich, Donald A. (Donald Arthur), 1943-
Kelm, Gary G.
Crooker, Andrew J. (Andrew Jackson), 1939-
Lewis Research Center.

January 1975

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

The effect of the inlet mach number and inlet-boundary-layer thickness on the performance of a 23©� conical-diffuser-tail-pipe combination /

Persh, Jerome.
Langley Aeronautical Laboratory.
United States. National Adviosry Committee for Aeronautics. NACA research memorandum.

January 1950

"March 21, 1950."Includes bibliographical references (p. 21).Mode of access: Internet

Experimental and analytical study of a conically diffused flow with a nearly separated boundary layer /

Boldman, Donald R.
Neumann, Harvey E.
Lewis Research Center.

January 1973

Prepared at Lewis Research Center.Cover title.Includes bibliographical references (p. 38-39).Mode of...

Effect of wall suction on performance of a short annular diffuser at inlet Mach numbers up to 0.5 /

Juhasz, Albert J.
Lewis Research Center.

January 1975

Prepared at Lewis Research Center.Cover title.Bibliography: p. 12-13.Mode of access: Internet

Design and experimental performance of short curved wall diffusers with axial symmetry utilizing slot suction /

Yang, Tah-teh.
Nelson, Carl D.
Hudson, William G.
Lewis Research Center.
Clemson University.

January 1973

"Prepared by Clemson University ... for Lewis Research Center."Cover title.Bibliography: p. 40.Mode ...

Effect of wall edge suction on the performance of a short annular dump diffuser with exit passage flow resistance

Juhasz, A. J.

April 1975

The effect of wall edge suction on the performance of a short annular dump diffuser having a perfora...

Performance of high-area-ratio annular dump diffuser using suction-stabilized-vortex flow control /

Juhasz, Albert J.
Smith, John M., joint author.
United States. National Aeronautics and Space Administration.

January 1977

Issued May 1977.Includes bibliographical references (p. 19).Mode of access: Internet

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...

Effects of suction boundary-layer control on the performance of a short annular diffuser with an upstream terminal normal shock /

Shoemaker, Charles J.
Henry, John R.
United States. National Aeronautics and Space Administration.

Cover title."April 1962."Aerodynamics, aircraft; Propulsion system elements; Propulsion systems, air...

Effect of inducer inlet and diffuser throat areas on performance of a low pressure ratio sweptback centrifugal compressor /

Klassen, Hugh A.
Lewis Research Center.

January 1975

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

Reduction of wind-tunnel wall interference by controlled wall flow /

Bernstein, Samuel.
Joppa, Robert G. (Robert Glenn)
University of Washington. Dept. of Aeronautics and Astronautics.
United States. National Aeronautics and Space Administration.

January 1976

Cover title.Includes bibliographical references (p. 47-49).Mode of access: Internet

Flow and wall-temperature sensitivity in parallel passages for large inlet to exit density ratios in subsonic flow /

Reshotko, Meyer.
Lewis Research Center.
United States. National Aeronautics and Space Administration.

January 1968

Cover title."July 1968."Includes bibliographical references (p. 28).Mode of access: Internet

An experimental study of near wall flow parameters in the blade end-wall corner region /

Bhargava, Rakesh K.
Raj, Rishi S.
Lewis Research Center.

January 1989

"Prepared for Lewis Research Center under Grant NAG3-122."Bibliography: p. 282-297.Mode of access: I...

An investigation of the flow characteristics in the blade endwall corner region /

Hazarika, Birinchi K.
Raj, Rishi.
Lewis Research Center.

January 1987

"July 1987"--Cover."Prepared for Lewis Research Center under Contract NAS3-122."Includes bibliograph...

Transonic off-design drag and performance of three mixed-compression axisymmetric inlets /

Woollett, Richard R.
Choby, David A.
Meleason, Edward T.
Lewis Research Center.

January 1975

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

Effect on fan flow characteristics of length and axial location of a cascade thrust reverser /

Dietrich, Donald A. (Donald Arthur), 1943-
Kelm, Gary G.
Crooker, Andrew J. (Andrew Jackson), 1939-
Lewis Research Center.

January 1975

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

The effect of the inlet mach number and inlet-boundary-layer thickness on the performance of a 23©� conical-diffuser-tail-pipe combination /

Persh, Jerome.
Langley Aeronautical Laboratory.
United States. National Adviosry Committee for Aeronautics. NACA research memorandum.

January 1950

"March 21, 1950."Includes bibliographical references (p. 21).Mode of access: Internet

Experimental and analytical study of a conically diffused flow with a nearly separated boundary layer /

Boldman, Donald R.
Neumann, Harvey E.
Lewis Research Center.

January 1973

Prepared at Lewis Research Center.Cover title.Includes bibliographical references (p. 38-39).Mode of...

Effect of wall edge suction on the performance of a short annular dump diffuser with exit passage flow resistance /

Abstract

Extracted data

Effect of wall edge suction on the performance of a short annular dump diffuser with exit passage flow resistance /

Abstract

Extracted data

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