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

Note on performance of aircraft ejector nozzles at high secondary flows /

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

On front cover: "August 27, 1954."Title from cover.Includes bibliographical references: p. 9.Mode of...

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...

Aerodynamic characteristics in ground effect of a large-scale model with a high disk-loading lifting fan mounted in the fuselage

deSavigny, Richard A.
Hickey, David H.
United States. National Aeronautics and Space Administration.

Cover title."January 1963."Includes bibliographical references.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...

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 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....

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...

Aerodynamic performance of axial-flow fan stage operated at nine inlet guide vane angles /

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

January 1979

"September 1979"--Cover.Includes bibliographical references (p. 12).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

Reduction of wind-tunnel wall interference by controlled wall flow /

Bernstein, Samuel.
Joppa, Robert G. (Robert Glenn)
University of Washington. Dept. of Aeronautics and Astronautics.
United States. National Aeronautics and Space Administration.

January 1976

Cover title.Includes bibliographical references (p. 47-49).Mode of access: Internet

Characteristics of loaded fan rotor blade wakes /

Reynolds, B.
Lakshminarayana, B.
Lewis Research Center.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.

January 1979

STAR category no. 02."October 1979"--Cover.Bibliography: p. 178-180.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...

Aerodynamics of a tilting ducted fan configuration /

Yaggy, Paul F.
Goodson, Kenneth W.
United States. National Aeronautics and Space Administration.

Cover title."March 1961."Aerodynamics, aircraft; Aircraft; Propulsion systems, air-jet; Stability an...

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...

Performance of two-stage fan with larger dampers on first-stage rotor /

Urasek, Donald C.
Lewis Research Center.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Office.

January 1979

"May 1979"--Cover."Lewis Research Center."Includes bibliographical references.Mode of access: Intern...

Note on performance of aircraft ejector nozzles at high secondary flows /

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

On front cover: "August 27, 1954."Title from cover.Includes bibliographical references: p. 9.Mode of...

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...

Aerodynamic characteristics in ground effect of a large-scale model with a high disk-loading lifting fan mounted in the fuselage

deSavigny, Richard A.
Hickey, David H.
United States. National Aeronautics and Space Administration.

Cover title."January 1963."Includes bibliographical references.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...

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 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....

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...

Aerodynamic performance of axial-flow fan stage operated at nine inlet guide vane angles /

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

January 1979

"September 1979"--Cover.Includes bibliographical references (p. 12).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

Reduction of wind-tunnel wall interference by controlled wall flow /

Bernstein, Samuel.
Joppa, Robert G. (Robert Glenn)
University of Washington. Dept. of Aeronautics and Astronautics.
United States. National Aeronautics and Space Administration.

January 1976

Cover title.Includes bibliographical references (p. 47-49).Mode of access: Internet

Characteristics of loaded fan rotor blade wakes /

Reynolds, B.
Lakshminarayana, B.
Lewis Research Center.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.

January 1979

STAR category no. 02."October 1979"--Cover.Bibliography: p. 178-180.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...

Aerodynamics of a tilting ducted fan configuration /

Yaggy, Paul F.
Goodson, Kenneth W.
United States. National Aeronautics and Space Administration.

Cover title."March 1961."Aerodynamics, aircraft; Aircraft; Propulsion systems, air-jet; Stability an...

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...

Performance of two-stage fan with larger dampers on first-stage rotor /

Urasek, Donald C.
Lewis Research Center.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Office.

January 1979

"May 1979"--Cover."Lewis Research Center."Includes bibliographical references.Mode of access: Intern...

Note on performance of aircraft ejector nozzles at high secondary flows /

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

On front cover: "August 27, 1954."Title from cover.Includes bibliographical references: p. 9.Mode of...

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...

Aerodynamic characteristics in ground effect of a large-scale model with a high disk-loading lifting fan mounted in the fuselage

deSavigny, Richard A.
Hickey, David H.
United States. National Aeronautics and Space Administration.

Cover title."January 1963."Includes bibliographical references.Mode of access: Internet

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

Abstract

Extracted data

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

Abstract

Extracted data

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