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

Analytical investigation of two liquid cooling systems for turbine blades /

Jackson, Thomas W.
Livingood, John N. B., joint author.
United States. National Advisory Committee for Aeronautics. NACA research memorandum.
Lewis Flight Propulsion Laboratory.

On front cover: "August 17, 1951."Title from cover.Includes bibliographical references: p. 19.Mode o...

Experimental investigation of the heat-transfer characteristics of an air-cooled sintered porous turbine blade /

Schafer, Louis J. Jr.
Richards, Hadley T., joint author.
Bartoo, Edward R., joint author.
United States. National Advisory Committee for Aeronautics. NACA research memorandum.
Lewis Flight Propulsion Laboratory.

On front cover: "February 5, 1952."Title from cover.Includes bibliographical references: p. 18-20.Mo...

Effects of increased leading-edge thickness on performance of a transonic rotor blade /

Reid, Lonnie.
Urasek, Donald C.
Lewis Research Center.

January 1973

Prepared at Lewis Research Center.Cover title.Includes bibliographical references (p. 19).Mode of ac...

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

Visualization of secondary-flow phenomena in blade row /

Herzig, H. Z.
Costello, G. R., joint author.
Hansen, A. G., joint author.
United States. National Advisory Committee for Aeronautics. NACA research memorandum.
Lewis Flight Propulsion Laboratory.

On front cover: "August 26, 1952."Title from cover.Includes bibliographical references: p. 8.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

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 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....

Influence of wall boundary layer upon the performance of an axial-flow fan rotor /

Boxer, Emanuel.
Langley Aeronautical Laboratory.
United States. National Adviosry Committee for Aeronautics. NACA research memorandum.

January 1947

"May 19, 1947"--Cover.Caption title.Includes bibliographical references (p. 8).Mode of access: Inter...

Analysis of factors affecting selection and design of air-cooled single-stage turbines for turbojet engines

Hubbartt, James E.
Schramm, Wilson B., joint author.
Rossbach, Richard J., joint author.
United States. National Advisory Committee for Aeronautics. NACA research memorandum.
Lewis Flight Propulsion Laboratory.

On front cover: "September 16, 1954."Title from cover.Includes bibliographical references: p. 24.Mod...

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

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

Effect of properties of primary fluid on performance of cylindrical shroud ejectors /

Kochendorfer, Fred D.
United States. National Advisory Committee for Aeronautics. NACA research memorandum.
Lewis Flight Propulsion Laboratory.

On front cover: "March 11, 1954."Title from cover.Includes bibliographical references: p. 16.Mode of...

Investigation of transonic turbine designed for zero diffusion of suction-surface velocity /

Whitney, Warren J.
Wong, Robert Y., joint author.
Monroe, Daniel E., joint author.
United States. National Advisory Committee for Aeronautics. NACA research memorandum.
Lewis Flight Propulsion Laboratory.

On front cover: "August 24, 1954."Title from cover.Includes bibliographical references: p. 9.Mode of...

Analytical investigation of two liquid cooling systems for turbine blades /

Jackson, Thomas W.
Livingood, John N. B., joint author.
United States. National Advisory Committee for Aeronautics. NACA research memorandum.
Lewis Flight Propulsion Laboratory.

On front cover: "August 17, 1951."Title from cover.Includes bibliographical references: p. 19.Mode o...

Experimental investigation of the heat-transfer characteristics of an air-cooled sintered porous turbine blade /

Schafer, Louis J. Jr.
Richards, Hadley T., joint author.
Bartoo, Edward R., joint author.
United States. National Advisory Committee for Aeronautics. NACA research memorandum.
Lewis Flight Propulsion Laboratory.

On front cover: "February 5, 1952."Title from cover.Includes bibliographical references: p. 18-20.Mo...

Effects of increased leading-edge thickness on performance of a transonic rotor blade /

Reid, Lonnie.
Urasek, Donald C.
Lewis Research Center.

January 1973

Prepared at Lewis Research Center.Cover title.Includes bibliographical references (p. 19).Mode of ac...

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

Visualization of secondary-flow phenomena in blade row /

Herzig, H. Z.
Costello, G. R., joint author.
Hansen, A. G., joint author.
United States. National Advisory Committee for Aeronautics. NACA research memorandum.
Lewis Flight Propulsion Laboratory.

On front cover: "August 26, 1952."Title from cover.Includes bibliographical references: p. 8.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

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 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....

Influence of wall boundary layer upon the performance of an axial-flow fan rotor /

Boxer, Emanuel.
Langley Aeronautical Laboratory.
United States. National Adviosry Committee for Aeronautics. NACA research memorandum.

January 1947

"May 19, 1947"--Cover.Caption title.Includes bibliographical references (p. 8).Mode of access: Inter...

Analysis of factors affecting selection and design of air-cooled single-stage turbines for turbojet engines

Hubbartt, James E.
Schramm, Wilson B., joint author.
Rossbach, Richard J., joint author.
United States. National Advisory Committee for Aeronautics. NACA research memorandum.
Lewis Flight Propulsion Laboratory.

On front cover: "September 16, 1954."Title from cover.Includes bibliographical references: p. 24.Mod...

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

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

Effect of properties of primary fluid on performance of cylindrical shroud ejectors /

Kochendorfer, Fred D.
United States. National Advisory Committee for Aeronautics. NACA research memorandum.
Lewis Flight Propulsion Laboratory.

On front cover: "March 11, 1954."Title from cover.Includes bibliographical references: p. 16.Mode of...

Investigation of transonic turbine designed for zero diffusion of suction-surface velocity /

Whitney, Warren J.
Wong, Robert Y., joint author.
Monroe, Daniel E., joint author.
United States. National Advisory Committee for Aeronautics. NACA research memorandum.
Lewis Flight Propulsion Laboratory.

On front cover: "August 24, 1954."Title from cover.Includes bibliographical references: p. 9.Mode of...

Analytical investigation of two liquid cooling systems for turbine blades /

Jackson, Thomas W.
Livingood, John N. B., joint author.
United States. National Advisory Committee for Aeronautics. NACA research memorandum.
Lewis Flight Propulsion Laboratory.

On front cover: "August 17, 1951."Title from cover.Includes bibliographical references: p. 19.Mode o...

Experimental investigation of the heat-transfer characteristics of an air-cooled sintered porous turbine blade /

Schafer, Louis J. Jr.
Richards, Hadley T., joint author.
Bartoo, Edward R., joint author.
United States. National Advisory Committee for Aeronautics. NACA research memorandum.
Lewis Flight Propulsion Laboratory.

On front cover: "February 5, 1952."Title from cover.Includes bibliographical references: p. 18-20.Mo...

Effects of increased leading-edge thickness on performance of a transonic rotor blade /

Reid, Lonnie.
Urasek, Donald C.
Lewis Research Center.

January 1973

Prepared at Lewis Research Center.Cover title.Includes bibliographical references (p. 19).Mode of ac...

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

Abstract

Extracted data

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

Abstract

Extracted data

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