Test-engine and inlet performance of an aircraft used for investigating flight effects on fan noise /

Aircraft noise prediction program user's manual /

Gillian, Ronnie E.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.
Langley Research Center.

January 1982

Subject category 71."Langley Research Center.""January 1983"--Cover.Distributed to depository librar...

Experimental study of noise reduction for an unstiffened cylindrical model of an airplane fuselage /

Willis, Conrad M.
Daniels, Edward F.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.
Langley Research Center.

January 1981

Subject category 71."Langley Research Center.""December 1981"--Cover.Includes bibliographical refere...

Flight effects on noise generated by the JT8D engine with inverted primary/fan flow as measured in the NASA-Ames 40- by 80-foot wind tunnel /

Strout, Frank G.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Office.
Boeing Commercial Airplane Company.

January 1978

June 1978.Contract NAS2-9302.Includes bibliographical references.Mode of access: Internet

Analysis of noise measured from a propeller in a wake /

Block, P. J. W.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.

January 1984

Subject category 71."November 1984"--Cover.Distributed to depository libraries in microfiche.Include...

Study of stator-vane fluctuating pressures in a turbofan engine for static and flight tests /

Mueller, Arnold W.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.

January 1984

Subject category 71."April 1984"--Cover.Distributed to depository libraries in microfiche.Includes b...

Propeller aircraft interior noise model /

Pope, L. D.
Wilby, John F.
Wilby, E. G.
Bolt, Beranek, and Newman, inc.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.
Langley Research Center.

January 1984

Subject category 71."July 1984"--Cover.Distributed to depository libraries in microfiche."Bolt Beran...

Fluctuating pressures on fan blades of a turbofan engine : flight test investigation /

Schoenster, James A.
Langley Research Center.

January 1985

Prepared at Langley Research Center."February 1985"--Cover.Includes bibliographical references (p. 7...

An experimental investigation of the aerodynamics and cooling of a horizontally-opposed air-cooled aircraft engine installation /

Miley, Stan J.
Langley Research Center.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.

January 1982

Subject category 02."March 1981"--Cover.Includes bibliographical references.Mode of access: Internet

Fluctuating pressures on fan blades of a turbofan engine : static and wind-tunnel investigations /

Schonester, James A.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.
Langley Research Center.

January 1982

Subject Category 71."March 1982"--Cover."Langley Research Center."Includes bibliographical reference...

Flight and wind-tunnel comparisons of the inlet/airframe interaction of the F-15 airplane /

Webb, Lannie D.
Whitmore, Stephen A.
Andriyich-Varda, Dom.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.

January 1984

STAR category 05.Distributed to depository libraries in microfiche."November 1984"--Cover.Bibliograp...

Investigation of jet-installation noise sources under static conditions /

Shearin, John G.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.

January 1983

Subject category 71."August 1983"--Cover.Distributed to depository libraries in microfiche.Includes ...

Measurement of performance, inlet flow characteristics, and radiated noise for a turbojet engine having choked inlet flow /

Cawthorn, Jimmy M.
Hayes, Clyde.
Morris, Garland J.
United States. National Aeronautics and Space Administration.
Langley Research Center.

January 1967

Performed at Langley Research Center."May 1967."Includes bibliographical references (p. 16).Mode of ...

Noise-reduction measurements on stiffened and unstiffened cylindrical models of an airplane fuselage /

Willis, Conrad M.
Mayes, William H.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Office.

January 1984

Subject category 71."February 1984"--Cover.Distributed to depository libraries in microfiche.Include...

Handbook of aircraft noise metrics /

Bennett, Ricarda L.
Pearsons, Karl S.
Langley Research Center.

January 1981

Subject category 71."March 1981"--Cover.Includes bibliographical references and index.Mode of access...

Ground and in-flight acoustic and performance characteristics of jet-aircraft exhaust noise supressors /

Coles, Willard D.
Swann, William H.
Mihaloew, John A,
United States. National Aeronautics and Space Administration.

Cover title."August 1961."Aerodynamics, aircraft; Aircraft; Aircraft safety and noise; Propulsion sy...

Aircraft noise prediction program user's manual /

Gillian, Ronnie E.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.
Langley Research Center.

January 1982

Subject category 71."Langley Research Center.""January 1983"--Cover.Distributed to depository librar...

Experimental study of noise reduction for an unstiffened cylindrical model of an airplane fuselage /

Willis, Conrad M.
Daniels, Edward F.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.
Langley Research Center.

January 1981

Subject category 71."Langley Research Center.""December 1981"--Cover.Includes bibliographical refere...

Flight effects on noise generated by the JT8D engine with inverted primary/fan flow as measured in the NASA-Ames 40- by 80-foot wind tunnel /

Strout, Frank G.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Office.
Boeing Commercial Airplane Company.

January 1978

June 1978.Contract NAS2-9302.Includes bibliographical references.Mode of access: Internet

Analysis of noise measured from a propeller in a wake /

Block, P. J. W.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.

January 1984

Subject category 71."November 1984"--Cover.Distributed to depository libraries in microfiche.Include...

Study of stator-vane fluctuating pressures in a turbofan engine for static and flight tests /

Mueller, Arnold W.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.

January 1984

Subject category 71."April 1984"--Cover.Distributed to depository libraries in microfiche.Includes b...

Propeller aircraft interior noise model /

Pope, L. D.
Wilby, John F.
Wilby, E. G.
Bolt, Beranek, and Newman, inc.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.
Langley Research Center.

January 1984

Subject category 71."July 1984"--Cover.Distributed to depository libraries in microfiche."Bolt Beran...

Fluctuating pressures on fan blades of a turbofan engine : flight test investigation /

Schoenster, James A.
Langley Research Center.

January 1985

Prepared at Langley Research Center."February 1985"--Cover.Includes bibliographical references (p. 7...

An experimental investigation of the aerodynamics and cooling of a horizontally-opposed air-cooled aircraft engine installation /

Miley, Stan J.
Langley Research Center.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.

January 1982

Subject category 02."March 1981"--Cover.Includes bibliographical references.Mode of access: Internet

Fluctuating pressures on fan blades of a turbofan engine : static and wind-tunnel investigations /

Schonester, James A.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.
Langley Research Center.

January 1982

Subject Category 71."March 1982"--Cover."Langley Research Center."Includes bibliographical reference...

Flight and wind-tunnel comparisons of the inlet/airframe interaction of the F-15 airplane /

Webb, Lannie D.
Whitmore, Stephen A.
Andriyich-Varda, Dom.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.

January 1984

STAR category 05.Distributed to depository libraries in microfiche."November 1984"--Cover.Bibliograp...

Investigation of jet-installation noise sources under static conditions /

Shearin, John G.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.

January 1983

Subject category 71."August 1983"--Cover.Distributed to depository libraries in microfiche.Includes ...

Measurement of performance, inlet flow characteristics, and radiated noise for a turbojet engine having choked inlet flow /

Cawthorn, Jimmy M.
Hayes, Clyde.
Morris, Garland J.
United States. National Aeronautics and Space Administration.
Langley Research Center.

January 1967

Performed at Langley Research Center."May 1967."Includes bibliographical references (p. 16).Mode of ...

Noise-reduction measurements on stiffened and unstiffened cylindrical models of an airplane fuselage /

Willis, Conrad M.
Mayes, William H.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Office.

January 1984

Subject category 71."February 1984"--Cover.Distributed to depository libraries in microfiche.Include...

Handbook of aircraft noise metrics /

Bennett, Ricarda L.
Pearsons, Karl S.
Langley Research Center.

January 1981

Subject category 71."March 1981"--Cover.Includes bibliographical references and index.Mode of access...

Ground and in-flight acoustic and performance characteristics of jet-aircraft exhaust noise supressors /

Coles, Willard D.
Swann, William H.
Mihaloew, John A,
United States. National Aeronautics and Space Administration.

Cover title."August 1961."Aerodynamics, aircraft; Aircraft; Aircraft safety and noise; Propulsion sy...

Aircraft noise prediction program user's manual /

Gillian, Ronnie E.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.
Langley Research Center.

January 1982

Subject category 71."Langley Research Center.""January 1983"--Cover.Distributed to depository librar...

Experimental study of noise reduction for an unstiffened cylindrical model of an airplane fuselage /

Willis, Conrad M.
Daniels, Edward F.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.
Langley Research Center.

January 1981

Subject category 71."Langley Research Center.""December 1981"--Cover.Includes bibliographical refere...

Flight effects on noise generated by the JT8D engine with inverted primary/fan flow as measured in the NASA-Ames 40- by 80-foot wind tunnel /

Strout, Frank G.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Office.
Boeing Commercial Airplane Company.

January 1978

June 1978.Contract NAS2-9302.Includes bibliographical references.Mode of access: Internet

Test-engine and inlet performance of an aircraft used for investigating flight effects on fan noise /

Abstract

Extracted data

Test-engine and inlet performance of an aircraft used for investigating flight effects on fan noise /

Abstract

Extracted data

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