Two-dimensional analytical and experimental performance comparison for a compressor stator section with d-factor of 0.47 /

Effect of casing treatment on overall and blade-element performance of a compressor rotor /

Moore, Royce D.
Blade, Robert J.
Kovich, George.
Ames Research Center.
United States. National Aeronautics and Space Administration.

January 1971

Prepared by Lewis Research Center."November 1971."N72-10025.Includes bibliographical references (p. ...

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)...

Performance of a highly loaded two-stage axial-flow fan /

Ruggeri, Robert S.
Benser, William A.
Lewis Research Center.

January 1974

Prepared at Lewis Research Center.Chiefly tables.Cover title.Mode of access: Internet

Comparison of two- and three-dimensional flow computations with laser anemometer measurements in a transonic compressor rotor /

Chima, Rodrick V.
Strazisar, Anthony J.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.

January 1982

STAR category 02."September 1982"--Cover.Includes bibliographical references.Mode of access: Interne...

Performance of inlet stage of transonic compressor /

Urasek, Donald C.
Lewis, George W., Jr.
Steinke, Ronald J.
Lewis Research Center.

January 1976

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

Effect of damper on overall and blade-element performance of a compressor rotor having a tip speed of 1151 feet per second and an aspect ratio of 3.6 /

Lewis, George W., Jr.
Hager, Roy D.
Lewis Research Center.

January 1974

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

Cold-air performance of compressor-drive turbine of Department of Energy upgraded automobile gas turbine engine /

Roelke, Richard J.
Haas, Jeffrey E.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.
Propulsion Laboratory (U.S.)
Lewis Research Center.

"October 1982"--Vol. II."Lewis Research Center.""June 1981"--Vol. I."AVRADCOM Research and Technolog...

Performance of single-stage axial-flow transonic compressor with rotor and stator aspect ratios of 1.63 and 1.78, respectively, and with design pressure ratio of 1.82 /

Moore, Royce D.
Reid, Lonnie.
Lewis Research Center.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.

January 1982

STAR category 07."Lewis Research Center.""February 1982"--Cover.Includes bibliographical references....

Performance of single-stage axial-flow transonic compressor with rotor and stator aspect ratios of 1.63 and 1.77, respectively, and with design pressure ratio of 2.05 /

Moore, Royce D.
Reid, Lonnie.
Lewis Research Center.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.

January 1982

STAR category 07."April 1982"--Cover."Lewis Research Center."Mode of access: Internet

Performance of a tandem-rotor/tandem-stator conical-flow compressor designed for a pressure ratio of 3 /

Wood, Jerry R.
Schumann, Lawrence F.
Owen, Albert Kimsey.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.

January 1982

"October 1982."STAR category 02.Distributed to depository libraries in microfiche.Includes bibliogra...

Stalled and stall-free performance of axial-flow compressor stage with three inlet-guide-vane and stator-blade settings /

Urasek, Donald C.
Cunnan, Walter S.
Steinke, Ronald J.
Lewis Research Center.

January 1977

Prepared at Lewis Research Center.Cover title.Includes bibliographical references (p. 13).Mode of ac...

Effect of slotted casing treatment on performance of a multistage compressor /

Moss, John E.
Lewis Research Center.

January 1976

Prepared at Lewis Research Center.Cover title.Includes bibliographical references (p. 10).Mode of ac...

FORTRAN program for predicting off-design performance of centrifugal compressors /

Galvas, Michael R.
U.S. Army Air Mobility Research and Development Laboratory.
Lewis Research Center.

January 1973

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

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...

Performance of vortex generators in a Mach 2.5 low-bleed full-scale 45-percent-internal-contraction axisymmetric inlet /

Neumann, Harvey E.
Shaw, Robert J. (Robert Joseph), 1946-
Wasserbauer, Joseph F.
Lewis Research Center.

January 1975

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

Effect of casing treatment on overall and blade-element performance of a compressor rotor /

Moore, Royce D.
Blade, Robert J.
Kovich, George.
Ames Research Center.
United States. National Aeronautics and Space Administration.

January 1971

Prepared by Lewis Research Center."November 1971."N72-10025.Includes bibliographical references (p. ...

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)...

Performance of a highly loaded two-stage axial-flow fan /

Ruggeri, Robert S.
Benser, William A.
Lewis Research Center.

January 1974

Prepared at Lewis Research Center.Chiefly tables.Cover title.Mode of access: Internet

Comparison of two- and three-dimensional flow computations with laser anemometer measurements in a transonic compressor rotor /

Chima, Rodrick V.
Strazisar, Anthony J.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.

January 1982

STAR category 02."September 1982"--Cover.Includes bibliographical references.Mode of access: Interne...

Performance of inlet stage of transonic compressor /

Urasek, Donald C.
Lewis, George W., Jr.
Steinke, Ronald J.
Lewis Research Center.

January 1976

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

Effect of damper on overall and blade-element performance of a compressor rotor having a tip speed of 1151 feet per second and an aspect ratio of 3.6 /

Lewis, George W., Jr.
Hager, Roy D.
Lewis Research Center.

January 1974

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

Cold-air performance of compressor-drive turbine of Department of Energy upgraded automobile gas turbine engine /

Roelke, Richard J.
Haas, Jeffrey E.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.
Propulsion Laboratory (U.S.)
Lewis Research Center.

"October 1982"--Vol. II."Lewis Research Center.""June 1981"--Vol. I."AVRADCOM Research and Technolog...

Performance of single-stage axial-flow transonic compressor with rotor and stator aspect ratios of 1.63 and 1.78, respectively, and with design pressure ratio of 1.82 /

Moore, Royce D.
Reid, Lonnie.
Lewis Research Center.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.

January 1982

STAR category 07."Lewis Research Center.""February 1982"--Cover.Includes bibliographical references....

Performance of single-stage axial-flow transonic compressor with rotor and stator aspect ratios of 1.63 and 1.77, respectively, and with design pressure ratio of 2.05 /

Moore, Royce D.
Reid, Lonnie.
Lewis Research Center.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.

January 1982

STAR category 07."April 1982"--Cover."Lewis Research Center."Mode of access: Internet

Performance of a tandem-rotor/tandem-stator conical-flow compressor designed for a pressure ratio of 3 /

Wood, Jerry R.
Schumann, Lawrence F.
Owen, Albert Kimsey.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.

January 1982

"October 1982."STAR category 02.Distributed to depository libraries in microfiche.Includes bibliogra...

Stalled and stall-free performance of axial-flow compressor stage with three inlet-guide-vane and stator-blade settings /

Urasek, Donald C.
Cunnan, Walter S.
Steinke, Ronald J.
Lewis Research Center.

January 1977

Prepared at Lewis Research Center.Cover title.Includes bibliographical references (p. 13).Mode of ac...

Effect of slotted casing treatment on performance of a multistage compressor /

Moss, John E.
Lewis Research Center.

January 1976

Prepared at Lewis Research Center.Cover title.Includes bibliographical references (p. 10).Mode of ac...

FORTRAN program for predicting off-design performance of centrifugal compressors /

Galvas, Michael R.
U.S. Army Air Mobility Research and Development Laboratory.
Lewis Research Center.

January 1973

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

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...

Performance of vortex generators in a Mach 2.5 low-bleed full-scale 45-percent-internal-contraction axisymmetric inlet /

Neumann, Harvey E.
Shaw, Robert J. (Robert Joseph), 1946-
Wasserbauer, Joseph F.
Lewis Research Center.

January 1975

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

Effect of casing treatment on overall and blade-element performance of a compressor rotor /

Moore, Royce D.
Blade, Robert J.
Kovich, George.
Ames Research Center.
United States. National Aeronautics and Space Administration.

January 1971

Prepared by Lewis Research Center."November 1971."N72-10025.Includes bibliographical references (p. ...

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)...

Performance of a highly loaded two-stage axial-flow fan /

Ruggeri, Robert S.
Benser, William A.
Lewis Research Center.

January 1974

Prepared at Lewis Research Center.Chiefly tables.Cover title.Mode of access: Internet

Two-dimensional analytical and experimental performance comparison for a compressor stator section with d-factor of 0.47 /

Abstract

Extracted data

Two-dimensional analytical and experimental performance comparison for a compressor stator section with d-factor of 0.47 /

Abstract

Extracted data

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