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

Experimental investigation of air-cooled turbine blades in turbojet engine

Esgar, Jack B.
Clure, John L., joint author.
United States. National Advisory Committee for Aeronautics. NACA research memorandum.
Lewis Flight Propulsion Laboratory.

On front cover: "May 8, 1952."Title from cover.Includes bibliographical references: p. 24-25.Mode of...

Performance of compressor blade cascades at high Mach numbers /

Bogdonoff, Seymour M.
Langley Aeronautical Laboratory.
United States. National Adviosry Committee for Aeronautics. NACA research memorandum.

January 1947

"June 12, 1947."Cover title.Includes bibliographical references (p. 12).Mode of access: Internet

Investigation of a gas turbine with National Bureau of Standards body 4811 ceramic rotor blades /

Freche, John C.
Sheflin, Bob W., joint author.
United States. National Advisory Committee for Aeronautics. NACA research memorandum.
United States. National Advisory Committee for Aeronautics.
Lewis Flight Propulsion Laboratory.

"October 28, 1948."Cover title.Includes bibliographical references (p. 12).Mode of access: Internet

Investigation of an impulse axial-flow compressor /

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

January 1950

"February 8, 1950."Includes bibliographical references (p. 22).Mode of access: Internet

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. ...

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...

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

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

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...

Experimental investigation of air-cooled turbine blades in turbojet engine

Hickel, Robert O.
Smith, Gordon T., joint author.
United States. National Advisory Committee for Aeronautics. NACA research memorandum.
Lewis Flight Propulsion Laboratory.

On front cover: "December 11, 1950."Title from cover.Includes bibliographical references: p. 15.Mode...

Investigations of air-cooled turbine rotors for turbojet engines

Nachtigall, Alfred J.
Ziemer, Robert R., joint author.
Zalabak, Charles F., joint author.
United States. National Advisory Committee for Aeronautics. NACA research memorandum.
Lewis Flight Propulsion Laboratory.

On front cover: "May 21, 1952."Title from cover.Includes bibliographical references: p. 22.Mode of a...

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

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

Experimental investigation of air-cooled turbine blades in turbojet engine

Stepka, Francis S.
Clure, John L., joint author.
Bear, H. Robert joint author.
United States. National Advisory Committee for Aeronautics. NACA research memorandum.
Lewis Flight Propulsion Laboratory.

On front cover: "September 24, 1954."Title from cover.Includes bibliographical references: p. 14-15....

Experimental investigation of air-cooled turbine blades in turbojet engine

Arne, Vernon L.
Esgar, Jack B., joint author.
United States. National Advisory Committee for Aeronautics. NACA research memorandum.
Lewis Flight Propulsion Laboratory.

On front cover: "April 2, 1951."Title from cover.Includes bibliographical references: p. 21.Mode of ...

Experimental investigation of air-cooled turbine blades in turbojet engine

Esgar, Jack B.
Clure, John L., joint author.
United States. National Advisory Committee for Aeronautics. NACA research memorandum.
Lewis Flight Propulsion Laboratory.

On front cover: "May 8, 1952."Title from cover.Includes bibliographical references: p. 24-25.Mode of...

Performance of compressor blade cascades at high Mach numbers /

Bogdonoff, Seymour M.
Langley Aeronautical Laboratory.
United States. National Adviosry Committee for Aeronautics. NACA research memorandum.

January 1947

"June 12, 1947."Cover title.Includes bibliographical references (p. 12).Mode of access: Internet

Investigation of a gas turbine with National Bureau of Standards body 4811 ceramic rotor blades /

Freche, John C.
Sheflin, Bob W., joint author.
United States. National Advisory Committee for Aeronautics. NACA research memorandum.
United States. National Advisory Committee for Aeronautics.
Lewis Flight Propulsion Laboratory.

"October 28, 1948."Cover title.Includes bibliographical references (p. 12).Mode of access: Internet

Investigation of an impulse axial-flow compressor /

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

January 1950

"February 8, 1950."Includes bibliographical references (p. 22).Mode of access: Internet

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. ...

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...

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

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

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...

Experimental investigation of air-cooled turbine blades in turbojet engine

Hickel, Robert O.
Smith, Gordon T., joint author.
United States. National Advisory Committee for Aeronautics. NACA research memorandum.
Lewis Flight Propulsion Laboratory.

On front cover: "December 11, 1950."Title from cover.Includes bibliographical references: p. 15.Mode...

Investigations of air-cooled turbine rotors for turbojet engines

Nachtigall, Alfred J.
Ziemer, Robert R., joint author.
Zalabak, Charles F., joint author.
United States. National Advisory Committee for Aeronautics. NACA research memorandum.
Lewis Flight Propulsion Laboratory.

On front cover: "May 21, 1952."Title from cover.Includes bibliographical references: p. 22.Mode of a...

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

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

Experimental investigation of air-cooled turbine blades in turbojet engine

Stepka, Francis S.
Clure, John L., joint author.
Bear, H. Robert joint author.
United States. National Advisory Committee for Aeronautics. NACA research memorandum.
Lewis Flight Propulsion Laboratory.

On front cover: "September 24, 1954."Title from cover.Includes bibliographical references: p. 14-15....

Experimental investigation of air-cooled turbine blades in turbojet engine

Arne, Vernon L.
Esgar, Jack B., joint author.
United States. National Advisory Committee for Aeronautics. NACA research memorandum.
Lewis Flight Propulsion Laboratory.

On front cover: "April 2, 1951."Title from cover.Includes bibliographical references: p. 21.Mode of ...

Experimental investigation of air-cooled turbine blades in turbojet engine

Esgar, Jack B.
Clure, John L., joint author.
United States. National Advisory Committee for Aeronautics. NACA research memorandum.
Lewis Flight Propulsion Laboratory.

On front cover: "May 8, 1952."Title from cover.Includes bibliographical references: p. 24-25.Mode of...

Performance of compressor blade cascades at high Mach numbers /

Bogdonoff, Seymour M.
Langley Aeronautical Laboratory.
United States. National Adviosry Committee for Aeronautics. NACA research memorandum.

January 1947

"June 12, 1947."Cover title.Includes bibliographical references (p. 12).Mode of access: Internet

Investigation of a gas turbine with National Bureau of Standards body 4811 ceramic rotor blades /

Freche, John C.
Sheflin, Bob W., joint author.
United States. National Advisory Committee for Aeronautics. NACA research memorandum.
United States. National Advisory Committee for Aeronautics.
Lewis Flight Propulsion Laboratory.

"October 28, 1948."Cover title.Includes bibliographical references (p. 12).Mode of access: Internet

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

Abstract

Extracted data

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

Abstract

Extracted data

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