Investigation of an impulse axial-flow compressor /

End wall flow characteristics and overall performance of an axial flow compressor stage /

Sitaram, N.
Lakshminarayana, B.
Pennsylvania State University.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.
Lewis Research Center.

January 1983

"February 1983"--Cover."Pennsylvania State University."Includes bibliographical references.Mode of a...

Some effects of blade trailing-edge thickness on performance of a single-stage axial-flow compressor /

Moses, J. J.
Serovy, G. K., joint author.
United States. National Advisory Committee for Aeronautics. NACA research memorandum.
Lewis Flight Propulsion Laboratory.

On front cover: "October 26, 1951."Title from cover.Includes bibliographical references: p. 7.Mode o...

Altitude-wind-tunnel investigation of a 4000-pound-thrust axial-flow turbojet engine

Fleming, William A.
United States. National Advisory Committee for Aeronautics. NACA research memorandum.
Flight Propulsion Research Laboratory.

On front cover: "August 3, 1948."Includes bibliographical references: p. 17.Mode of access: Internet

Investigation of an impulse axial-flow compressor rotor over a range of blade angles /

Schulze, Wallace M.
Westphal, Willard R.
Erwin, John R.
Langley Aeronautical Laboratory.
United States. National Adviosry Committee for Aeronautics. NACA research memorandum.

January 1950

"August 29, 1950."Cover title.Includes bibliographical references (p. 16).Mode of access: Internet

Experimental investigation of an axial-flow supersonic compressor having sharp leading-edge blades with an 8-percent mean thickness-chord ratio /

Goldberg, Theodore J.
Langley Aeronautical Laboratory.
United States. National Adviosry Committee for Aeronautics. NACA research memorandum.

January 1955

"February 4, 1955."Includes bibliographical references (p. 12).Mode of access: Internet

Research on rotating stall in axial flow compressors.

Moore, F. K.
Armed Services Technical Information Agency (U.S.)
Wright Air Development Center.

"January 1959."Includes bibliographical references (p. 16).Mode of access: Internet

Low-speed cascade investigation of loaded leading-edge compressor blades /

Emery, James C.
Langley Aeronautical Laboratory.
United States. National Adviosry Committee for Aeronautics. NACA research memorandum.

January 1956

"January 11, 1956."Includes bibliographical references (p. 11).Mode of access: Internet

Vibration survey of blades in 10-stage axial-flow compressor

Meyer, Andre J. Jr.
Calvert, Howard F., joint author.
United States. National Advisory Committee for Aeronautics. NACA research memorandum.
Lewis Flight Propulsion Laboratory.

On front cover: "January 31, 1949."Includes bibliographical references: p. 6.Mode of access: Interne...

Experimental investigation of a transonic axial-flow-compressor rotor with double-circular-arc airfoil blade sections.

Lewis, George W., Jr.
Serovy, G. K. (George K.)
Schwenk, Francis C.
Lewis Flight Propulsion Laboratory.
United States. National Adviosry Committee for Aeronautics. NACA research memorandum.

January 1954

"Declassified October 31, 1958.""April 5, 1954."Cover title.Includes bibliographical references (p. ...

Rotating stall investigation of the 0.72 hub-tip ratio single-stage compressor /

Graham, Robert W.
Prian, Vasily D.
Lewis Flight Propulsion Laboratory.
United States. National Adviosry Committee for Aeronautics. NACA research memorandum.

January 1954

"March 9, 1954."Includes bibliographical references (p. 10-11).Mode of access: Internet

Investigation of the performance of a turbojet engine with variable-position compressor inlet guide vanes /

Budinger, Ray E.
Kaufman, Harold R.
Lewis Flight Propulsion Laboratory.
United States. National Adviosry Committee for Aeronautics. NACA research memorandum.

January 1955

"October 4, 1955."Includes bibliographical references (p. 20).Mode of access: Internet

Compressor-blade vibration of a J57-P-1 turbojet engine during exploratory operation with inlet-pressure distortions /

Hanson, Morgan P.
Lewis Flight Propulsion Laboratory.
United States. National Adviosry Committee for Aeronautics. NACA research memorandum.

January 1955

"December 23,1955."Includes bibliographical references (p. 11).Mode of access: Internet

Analysis of internal flow of J85-13 multistage compressor /

Hager, Roy D.
United States. National Aeronautics and Space Administration.

January 1977

Issued Apr. 1977.Includes bibliographical references (p. 7).Mode of access: Internet

A comparison of typical National Gas Turbine Establishment and NACA axial-flow compressor blade sections in cascade at low speed /

Felix, A. Richard.
Emery, James C.
Langley Aeronautical Laboratory.
United States. National Adviosry Committee for Aeronautics. NACA research memorandum.

January 1953

"May 1, 1953."Includes bibliographical references (p. 23).Mode of access: Internet

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

End wall flow characteristics and overall performance of an axial flow compressor stage /

Sitaram, N.
Lakshminarayana, B.
Pennsylvania State University.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.
Lewis Research Center.

January 1983

"February 1983"--Cover."Pennsylvania State University."Includes bibliographical references.Mode of a...

Some effects of blade trailing-edge thickness on performance of a single-stage axial-flow compressor /

Moses, J. J.
Serovy, G. K., joint author.
United States. National Advisory Committee for Aeronautics. NACA research memorandum.
Lewis Flight Propulsion Laboratory.

On front cover: "October 26, 1951."Title from cover.Includes bibliographical references: p. 7.Mode o...

Altitude-wind-tunnel investigation of a 4000-pound-thrust axial-flow turbojet engine

Fleming, William A.
United States. National Advisory Committee for Aeronautics. NACA research memorandum.
Flight Propulsion Research Laboratory.

On front cover: "August 3, 1948."Includes bibliographical references: p. 17.Mode of access: Internet

Investigation of an impulse axial-flow compressor rotor over a range of blade angles /

Schulze, Wallace M.
Westphal, Willard R.
Erwin, John R.
Langley Aeronautical Laboratory.
United States. National Adviosry Committee for Aeronautics. NACA research memorandum.

January 1950

"August 29, 1950."Cover title.Includes bibliographical references (p. 16).Mode of access: Internet

Experimental investigation of an axial-flow supersonic compressor having sharp leading-edge blades with an 8-percent mean thickness-chord ratio /

Goldberg, Theodore J.
Langley Aeronautical Laboratory.
United States. National Adviosry Committee for Aeronautics. NACA research memorandum.

January 1955

"February 4, 1955."Includes bibliographical references (p. 12).Mode of access: Internet

Research on rotating stall in axial flow compressors.

Moore, F. K.
Armed Services Technical Information Agency (U.S.)
Wright Air Development Center.

"January 1959."Includes bibliographical references (p. 16).Mode of access: Internet

Low-speed cascade investigation of loaded leading-edge compressor blades /

Emery, James C.
Langley Aeronautical Laboratory.
United States. National Adviosry Committee for Aeronautics. NACA research memorandum.

January 1956

"January 11, 1956."Includes bibliographical references (p. 11).Mode of access: Internet

Vibration survey of blades in 10-stage axial-flow compressor

Meyer, Andre J. Jr.
Calvert, Howard F., joint author.
United States. National Advisory Committee for Aeronautics. NACA research memorandum.
Lewis Flight Propulsion Laboratory.

On front cover: "January 31, 1949."Includes bibliographical references: p. 6.Mode of access: Interne...

Experimental investigation of a transonic axial-flow-compressor rotor with double-circular-arc airfoil blade sections.

Lewis, George W., Jr.
Serovy, G. K. (George K.)
Schwenk, Francis C.
Lewis Flight Propulsion Laboratory.
United States. National Adviosry Committee for Aeronautics. NACA research memorandum.

January 1954

"Declassified October 31, 1958.""April 5, 1954."Cover title.Includes bibliographical references (p. ...

Rotating stall investigation of the 0.72 hub-tip ratio single-stage compressor /

Graham, Robert W.
Prian, Vasily D.
Lewis Flight Propulsion Laboratory.
United States. National Adviosry Committee for Aeronautics. NACA research memorandum.

January 1954

"March 9, 1954."Includes bibliographical references (p. 10-11).Mode of access: Internet

Investigation of the performance of a turbojet engine with variable-position compressor inlet guide vanes /

Budinger, Ray E.
Kaufman, Harold R.
Lewis Flight Propulsion Laboratory.
United States. National Adviosry Committee for Aeronautics. NACA research memorandum.

January 1955

"October 4, 1955."Includes bibliographical references (p. 20).Mode of access: Internet

Compressor-blade vibration of a J57-P-1 turbojet engine during exploratory operation with inlet-pressure distortions /

Hanson, Morgan P.
Lewis Flight Propulsion Laboratory.
United States. National Adviosry Committee for Aeronautics. NACA research memorandum.

January 1955

"December 23,1955."Includes bibliographical references (p. 11).Mode of access: Internet

Analysis of internal flow of J85-13 multistage compressor /

Hager, Roy D.
United States. National Aeronautics and Space Administration.

January 1977

Issued Apr. 1977.Includes bibliographical references (p. 7).Mode of access: Internet

A comparison of typical National Gas Turbine Establishment and NACA axial-flow compressor blade sections in cascade at low speed /

Felix, A. Richard.
Emery, James C.
Langley Aeronautical Laboratory.
United States. National Adviosry Committee for Aeronautics. NACA research memorandum.

January 1953

"May 1, 1953."Includes bibliographical references (p. 23).Mode of access: Internet

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

End wall flow characteristics and overall performance of an axial flow compressor stage /

Sitaram, N.
Lakshminarayana, B.
Pennsylvania State University.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.
Lewis Research Center.

January 1983

"February 1983"--Cover."Pennsylvania State University."Includes bibliographical references.Mode of a...

Some effects of blade trailing-edge thickness on performance of a single-stage axial-flow compressor /

Moses, J. J.
Serovy, G. K., joint author.
United States. National Advisory Committee for Aeronautics. NACA research memorandum.
Lewis Flight Propulsion Laboratory.

On front cover: "October 26, 1951."Title from cover.Includes bibliographical references: p. 7.Mode o...

Altitude-wind-tunnel investigation of a 4000-pound-thrust axial-flow turbojet engine

Fleming, William A.
United States. National Advisory Committee for Aeronautics. NACA research memorandum.
Flight Propulsion Research Laboratory.

On front cover: "August 3, 1948."Includes bibliographical references: p. 17.Mode of access: Internet

Investigation of an impulse axial-flow compressor /

Abstract

Extracted data

Investigation of an impulse axial-flow compressor /

Abstract

Extracted data

Related items

Related items