Performance of inlet stage of transonic compressor /

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...

Performance of a turbojet engine in combination with an external-internal-compression inlet to mach 2.88 /

Bowditch, David N.
Tabata, William K.
Anderson, Bernhard H.
United States. National Aeronautics and Space Administration.

"July 1960."Cover title.Includes bibliographical references (p. 10-11).Mode of access: Internet

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....

Effect of casing treatment on performance of an inlet stage for a transonic multistage compressor /

Urasek, Donald C.
Moore, Royce D., joint author.
Lewis, George W., Jr, joint author.
Lewis Research Center.

January 1976

Cover title.Includes bibliographical references (p. 18).Mode of access: Internet

Performance of a 1.57-pressure-ratio transonic fan stage with a screen-induced 90 ̊circumferential inlet flow distribution /

Sanger, Nelson L.
Lewis Research Center.

January 1976

Prepared at Lewis Research Center.Cover title.Includes bibliographical references (p. 28).Mode of ac...

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...

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...

Transonic performance of a Mach 2.65 auxiliary flow axisymmetric inlet /

Santman, Don M.
United States. National Aeronautics and Space Administration.
Ames Research Center.
Ellco Engineering, Inc.

January 1976

Issued Oct. 1976.Cover title.Includes bibliographical references (p. 16).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)...

Experimental investigation of a transonic compressor cascade and test results for four blade sections /

Emery, James C.
Westphal, Willard R.
Dunavant, James C.
United States. National Aeronautics and Space Administration.

"January 1960."Cover title.Includes bliographical references (p. 10).Mode of access: Internet

Aerodynamic performance of a 1.25-pressure-ratio axial-flow fan stage /

Moore, Royce D.
Steinke, Ronald J.
Lewis Research Center.

January 1974

Prepared at Lewis Research Center.Chiefly tables.Cover title.Bibliography: p. 19.Mode of access: Int...

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 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

Design of 9.271-pressure-ratio five-stage core compressor and overall performance for first three stages /

Steinke, Ronald J.
Lewis Research Center.

January 1986

Prepared at Lewis Research Center."May 1986"--Cover.Includes bibliographical references (p. 16).Mode...

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

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...

Performance of a turbojet engine in combination with an external-internal-compression inlet to mach 2.88 /

Bowditch, David N.
Tabata, William K.
Anderson, Bernhard H.
United States. National Aeronautics and Space Administration.

"July 1960."Cover title.Includes bibliographical references (p. 10-11).Mode of access: Internet

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....

Effect of casing treatment on performance of an inlet stage for a transonic multistage compressor /

Urasek, Donald C.
Moore, Royce D., joint author.
Lewis, George W., Jr, joint author.
Lewis Research Center.

January 1976

Cover title.Includes bibliographical references (p. 18).Mode of access: Internet

Performance of a 1.57-pressure-ratio transonic fan stage with a screen-induced 90 ̊circumferential inlet flow distribution /

Sanger, Nelson L.
Lewis Research Center.

January 1976

Prepared at Lewis Research Center.Cover title.Includes bibliographical references (p. 28).Mode of ac...

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...

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...

Transonic performance of a Mach 2.65 auxiliary flow axisymmetric inlet /

Santman, Don M.
United States. National Aeronautics and Space Administration.
Ames Research Center.
Ellco Engineering, Inc.

January 1976

Issued Oct. 1976.Cover title.Includes bibliographical references (p. 16).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)...

Experimental investigation of a transonic compressor cascade and test results for four blade sections /

Emery, James C.
Westphal, Willard R.
Dunavant, James C.
United States. National Aeronautics and Space Administration.

"January 1960."Cover title.Includes bliographical references (p. 10).Mode of access: Internet

Aerodynamic performance of a 1.25-pressure-ratio axial-flow fan stage /

Moore, Royce D.
Steinke, Ronald J.
Lewis Research Center.

January 1974

Prepared at Lewis Research Center.Chiefly tables.Cover title.Bibliography: p. 19.Mode of access: Int...

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 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

Design of 9.271-pressure-ratio five-stage core compressor and overall performance for first three stages /

Steinke, Ronald J.
Lewis Research Center.

January 1986

Prepared at Lewis Research Center."May 1986"--Cover.Includes bibliographical references (p. 16).Mode...

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

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...

Performance of a turbojet engine in combination with an external-internal-compression inlet to mach 2.88 /

Bowditch, David N.
Tabata, William K.
Anderson, Bernhard H.
United States. National Aeronautics and Space Administration.

"July 1960."Cover title.Includes bibliographical references (p. 10-11).Mode of access: Internet

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 inlet stage of transonic compressor /

Abstract

Extracted data

Performance of inlet stage of transonic compressor /

Abstract

Extracted data

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