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

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...

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

The effect of wind-tunnel wall interference on the performance of a fan-in-wing VTOL model /

Heyson, Harry H.
Langley Research Center.

January 1974

Prepared at Langley Research Center.Cover title.Includes bibliographical references (p. 66-69).Mode ...

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

Juhasz, Albert J.
Lewis Research Center.

January 1975

Prepared at Lewis Research Center.Cover title.Includes bibliographical references (p. 16-17).Mode of...

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...

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

Juhasz, A. J.

October 1975

A short annular diffuser equipped with wall bleed (suction)capability was evaluated at inlet Mach nu...

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...

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

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...

Pressure recovery performance of conical diffusers at high subsonic Mach numbers /

Dolan, Francis X.
Runstadler, Peter W.
Lewis Research Center.
Creare, inc.

January 1973

"Prepared by Creare Incorporated ... for Lewis Research Center."Cover title.Bibliography: p. 142-143...

Effect of treated length on performance of full-scale turbofan inlet noise suppressors /

Dittmar, James H.
Groeneweg, John F. (John Frederick), 1937-
Lewis Research Center.

January 1974

Prepared at Lewis Research Center.Cover title.Includes bibliographical references (p. 14-15).Mode of...

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

The effects of boundary-layer removal through throat slots on the internal performance of a side inlet at Mach numbers of 2.0 and 2.3 /

Gawienowski, John J.
Ames Research Center.

January 1961

"March 1961."Cover title.Includes bibliographical references (p. 8).Mode of access: Internet

Low-speed performance of an axisymmetric, mixed-compression, supersonic inlet with auxiliary inlets /

Trefny, Charles J.
Wasserbauer, Joseph W.
Lewis Research Center.

January 1986

Prepared at Lewis Research Center."February 1986"--Cover.Includes bibliographical references (p. 10)...

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...

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

The effect of wind-tunnel wall interference on the performance of a fan-in-wing VTOL model /

Heyson, Harry H.
Langley Research Center.

January 1974

Prepared at Langley Research Center.Cover title.Includes bibliographical references (p. 66-69).Mode ...

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

Juhasz, Albert J.
Lewis Research Center.

January 1975

Prepared at Lewis Research Center.Cover title.Includes bibliographical references (p. 16-17).Mode of...

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...

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

Juhasz, A. J.

October 1975

A short annular diffuser equipped with wall bleed (suction)capability was evaluated at inlet Mach nu...

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...

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

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...

Pressure recovery performance of conical diffusers at high subsonic Mach numbers /

Dolan, Francis X.
Runstadler, Peter W.
Lewis Research Center.
Creare, inc.

January 1973

"Prepared by Creare Incorporated ... for Lewis Research Center."Cover title.Bibliography: p. 142-143...

Effect of treated length on performance of full-scale turbofan inlet noise suppressors /

Dittmar, James H.
Groeneweg, John F. (John Frederick), 1937-
Lewis Research Center.

January 1974

Prepared at Lewis Research Center.Cover title.Includes bibliographical references (p. 14-15).Mode of...

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

The effects of boundary-layer removal through throat slots on the internal performance of a side inlet at Mach numbers of 2.0 and 2.3 /

Gawienowski, John J.
Ames Research Center.

January 1961

"March 1961."Cover title.Includes bibliographical references (p. 8).Mode of access: Internet

Low-speed performance of an axisymmetric, mixed-compression, supersonic inlet with auxiliary inlets /

Trefny, Charles J.
Wasserbauer, Joseph W.
Lewis Research Center.

January 1986

Prepared at Lewis Research Center."February 1986"--Cover.Includes bibliographical references (p. 10)...

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...

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

The effect of wind-tunnel wall interference on the performance of a fan-in-wing VTOL model /

Heyson, Harry H.
Langley Research Center.

January 1974

Prepared at Langley Research Center.Cover title.Includes bibliographical references (p. 66-69).Mode ...

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

Abstract

Extracted data

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

Abstract

Extracted data

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