Experimental investigation of shock-cell noise reduction for dual-stream nozzles in simulated flight /

Evaluation of a telemetry system for use in shock interaction experiments /

Merritt, David L., author.
Aronson, Philip M., author.
Naval Ordnance Laboratory (White Oak, Md.)

The ability of the Miniature Telemetry System to measure transient pressures on a model flying throu...

Flight velocity effects on jet noise of several variations of a 48-tube suppressor installed on a plug nozzle /

Burley, Richard R.
Head, Verlon L.
Lewis Research Center.

January 1974

Prepared at Lewis Research Center.Cover title.Includes bibliographical references (p. 17-18).Mode of...

Investigation of sonic boom generated by thin, nonlifting, rectangular wings /

Davis, Sanford S.
Ames Research Center.
United States. National Aeronautics and Space Administration.

January 1971

Prepared by Ames Research Center."December 1971."N72-11949.Includes bibliographical references (p. 1...

Experimental investigation of shock-cell noise reduction for single-stream nozzles in simulated flight /

Yamamoto, K.
Lewis Research Center.
General Electric Company. Aircraft Engine Business Group.

January 1984

"Prepared [at GE Aircraft Engine Business Group] for Lewis Research Center under contract NAS3-22514...

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...

Experimental investigation of shock-cell noise reduction for dual-stream nozzles in simulated flight comprehensive data report. Volume 1: Test nozzles and acoustic data

Janardan, B. A.
Yamamoto, K.
Brausch, J. F.
Hoerst, D. J.
Price, A. O.

February 1984

Parameters which contribute to supersonic jet shock noise were investigated for the purpose of deter...

Analytical investigation of synchrophasing as a means of reducing aircraft interior noise /

Fuller, C. R.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.
Virginia Polytechnic Institute and State University.
Langley Research Center.

January 1984

"August 1984"--Cover.Subject category 71.Distributed to depository libraries in microfiche."Virginia...

Experimental investigation of shock-cell noise reduction for single-stream nozzles in simulated flight, comprehensive data report. Volume 3: Shadowgraph photos and facility description

Hoerst, D. J.
Price, A. O.
Yamamoto, K.
Knott, P. R.
Janardan, B. A.
Brausch, J. F.

May 1984

A total of 142 shadowgraph photographs were taken on 43 different plumes that were distributed over ...

Shock associated noise reduction from inverted-velcoity-profile coannular jets /

Tanna, H. K.
Brown, W. H.
Tam, C. K. W.
Langley Research Center.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.

January 1981

"August 1981"--Cover.Includes bibliographical references.Mode of access: Internet

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...

Refinement and application of acoustic impulse technique to study nozzle transmission characteristics /

Salikuddin, M.
Lewis Research Center.
Lockheed-Georgia Company.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.

January 1983

STAR category 7l."February 1983"--Cover."Lockheed-Georgia Company."Includes bibliographical referenc...

Theoretical and experimental investigation of supersonic aerodynamic characteristics of a twin-fuselage concept /

Wood, Richard M.
Brentner, Kenneth S.
Miller, D. S. (David S.)
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.

January 1983

Distributed to depository libraries in microfiche."August 1983"--Cover.Subject category 02.Includes ...

Effect of multiple-nozzle geometry on jet noise generation. /

Rollin, Vern G.
United States. National Aeronautics and Space Administration.

Cover title."September 1961."Aerodynamics, aircraft; Aerodynamics, missiles and space vehicles; Airc...

High velocity jet noise source location and reduction.

Savell, C. T.
United States. Federal Aviation Administration. Systems Research and Development Service.
General Electric Company. Advanced Engineering and Technology Program Department.

"February 22, 1977."Prepared by C.T. Savell et al. (General Electric Company, Advanced Engineering a...

An experimental study of the validity of the heat-field concept for sonic-boom alleviation /

Swigart, Rudolph J.
Langley Research Center.
Aerospace Corporation.

"Prepared by the Aerospace Corporation ... for Langley Research Center.""March 1974."Cover title.Inc...

Evaluation of a telemetry system for use in shock interaction experiments /

Merritt, David L., author.
Aronson, Philip M., author.
Naval Ordnance Laboratory (White Oak, Md.)

The ability of the Miniature Telemetry System to measure transient pressures on a model flying throu...

Flight velocity effects on jet noise of several variations of a 48-tube suppressor installed on a plug nozzle /

Burley, Richard R.
Head, Verlon L.
Lewis Research Center.

January 1974

Prepared at Lewis Research Center.Cover title.Includes bibliographical references (p. 17-18).Mode of...

Investigation of sonic boom generated by thin, nonlifting, rectangular wings /

Davis, Sanford S.
Ames Research Center.
United States. National Aeronautics and Space Administration.

January 1971

Prepared by Ames Research Center."December 1971."N72-11949.Includes bibliographical references (p. 1...

Experimental investigation of shock-cell noise reduction for single-stream nozzles in simulated flight /

Yamamoto, K.
Lewis Research Center.
General Electric Company. Aircraft Engine Business Group.

January 1984

"Prepared [at GE Aircraft Engine Business Group] for Lewis Research Center under contract NAS3-22514...

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...

Experimental investigation of shock-cell noise reduction for dual-stream nozzles in simulated flight comprehensive data report. Volume 1: Test nozzles and acoustic data

Janardan, B. A.
Yamamoto, K.
Brausch, J. F.
Hoerst, D. J.
Price, A. O.

February 1984

Parameters which contribute to supersonic jet shock noise were investigated for the purpose of deter...

Analytical investigation of synchrophasing as a means of reducing aircraft interior noise /

Fuller, C. R.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.
Virginia Polytechnic Institute and State University.
Langley Research Center.

January 1984

"August 1984"--Cover.Subject category 71.Distributed to depository libraries in microfiche."Virginia...

Experimental investigation of shock-cell noise reduction for single-stream nozzles in simulated flight, comprehensive data report. Volume 3: Shadowgraph photos and facility description

Hoerst, D. J.
Price, A. O.
Yamamoto, K.
Knott, P. R.
Janardan, B. A.
Brausch, J. F.

May 1984

A total of 142 shadowgraph photographs were taken on 43 different plumes that were distributed over ...

Shock associated noise reduction from inverted-velcoity-profile coannular jets /

Tanna, H. K.
Brown, W. H.
Tam, C. K. W.
Langley Research Center.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.

January 1981

"August 1981"--Cover.Includes bibliographical references.Mode of access: Internet

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...

Refinement and application of acoustic impulse technique to study nozzle transmission characteristics /

Salikuddin, M.
Lewis Research Center.
Lockheed-Georgia Company.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.

January 1983

STAR category 7l."February 1983"--Cover."Lockheed-Georgia Company."Includes bibliographical referenc...

Theoretical and experimental investigation of supersonic aerodynamic characteristics of a twin-fuselage concept /

Wood, Richard M.
Brentner, Kenneth S.
Miller, D. S. (David S.)
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.

January 1983

Distributed to depository libraries in microfiche."August 1983"--Cover.Subject category 02.Includes ...

Effect of multiple-nozzle geometry on jet noise generation. /

Rollin, Vern G.
United States. National Aeronautics and Space Administration.

Cover title."September 1961."Aerodynamics, aircraft; Aerodynamics, missiles and space vehicles; Airc...

High velocity jet noise source location and reduction.

Savell, C. T.
United States. Federal Aviation Administration. Systems Research and Development Service.
General Electric Company. Advanced Engineering and Technology Program Department.

"February 22, 1977."Prepared by C.T. Savell et al. (General Electric Company, Advanced Engineering a...

An experimental study of the validity of the heat-field concept for sonic-boom alleviation /

Swigart, Rudolph J.
Langley Research Center.
Aerospace Corporation.

"Prepared by the Aerospace Corporation ... for Langley Research Center.""March 1974."Cover title.Inc...

Evaluation of a telemetry system for use in shock interaction experiments /

Merritt, David L., author.
Aronson, Philip M., author.
Naval Ordnance Laboratory (White Oak, Md.)

The ability of the Miniature Telemetry System to measure transient pressures on a model flying throu...

Flight velocity effects on jet noise of several variations of a 48-tube suppressor installed on a plug nozzle /

Burley, Richard R.
Head, Verlon L.
Lewis Research Center.

January 1974

Prepared at Lewis Research Center.Cover title.Includes bibliographical references (p. 17-18).Mode of...

Investigation of sonic boom generated by thin, nonlifting, rectangular wings /

Davis, Sanford S.
Ames Research Center.
United States. National Aeronautics and Space Administration.

January 1971

Prepared by Ames Research Center."December 1971."N72-11949.Includes bibliographical references (p. 1...

Experimental investigation of shock-cell noise reduction for dual-stream nozzles in simulated flight /

Abstract

Extracted data

Experimental investigation of shock-cell noise reduction for dual-stream nozzles in simulated flight /

Abstract

Extracted data

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