Development of acoustically lined ejector technology for multitube jet noise suppressor nozzles by model and engine tests over a wide range of jet pressure ratios and temperatures /

NASA research on noise-abatement approach profiles for multiengine jet transport aircraft /

Zalovcik, John A.
Schaefer, William T., Jr.
United States. National Aeronautics and Space Administration.
Langley Research Center.

January 1967

Work performed at Langley Research Center."June 1967."Includes bibliographical references (p. 14).Mo...

Numerical study of sound propagation in a jet flow /

Padula, Sharon L.
Liu, Chen-Huei.
Langley Research Center.

January 1975

Prepared at Langley Research Center.Cover title.Includes bibliographical references (p. 20).Mode of ...

A methodology for designing aircraft to low sonic boom constraints /

Mack, Robert J.
Needleman, Kathy E.
Langley Research Center.

January 1991

Prepared at Langley Research Center.Includes bibliographical references (p. 6).Mode of access: Inter...

Developmental design, fabrication, and test of acoustic suppressors for fans of high bypass turbofan engines /

Tucker, R. H.
Lewis Research Center.
Boeing Company. Wichita Division.

January 1974

"Prepared by the Boeing Company, Wichita, Kans. ... for Lewis Research Center."Cover title.Bibliogra...

Study and development of acoustic treatment for jet engine tailpipes /

Nelsen, M. D.
Langley Research Center.
Boeing Company. AVCO Corporation. Systems Division.
United States. National Aeronautics and Space Administration.

January 1971

Prepared by The Boeing Company for Langley Research Center.N72-10043.Includes bibliographical refere...

Cold-flow acoustic evaluation of a small-scale, divergent, lobed nozzle for supersonic jet noise suppression /

Huff, Ronald G.
Groesbeck, Donald E.
Lewis Research Center.

January 1975

Prepared at Lewis Research Center.Cover title.Includes bibliographical references (p. 23).Mode of ac...

Reduction of acoustic disturbances in the test section of supersonic wind tunnels by laminarizing their nozzle and test section wall boundary layers by means of suction /

Pfenninger, W.
Syberg, J.
Langley Research Center.
Boeing Commercial Airplane Company.

January 1974

"Prepared by Boeing Commercial Airplane Company ... for Langley Research Center."Cover title.Include...

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

Burley, Richard R.
Johns, Albert L.
Lewis Research Center.

January 1974

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

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...

Flight velocity effects on the jet noise of several variations of a 104-tube suppressor nozzle /

Burley, Richard R.
Lewis Research Center.

January 1974

Prepared at Lewis Research Center.Cover title.Includes bibliographical references (p. 23-24).Mode of...

Design of a bleed system for a Mach 3.5 inlet /

Syberg, J.
Hickcox, T. E.
Ames Research Center.
Boeing Company.

January 1973

"Prepared by the Boeing Company ... for Ames Research Center."Cover title.Bibliography: p. 32.Mode o...

Dispersion of turbojet engine exhaust in flight /

Holdeman, James D.
Lewis Research Center.

January 1973

Prepared at Lewis Research Center.Cover title.Includes bibliographical references (p. 15).Mode of ac...

Assessment of an analytical procedure for predicting supersonic ejector nozzle performance /

Anderson, Bernhard H.
Lewis Research Center.

January 1974

Prepared at Lewis Research Center.Cover title.Includes bibliographical references (p. 13-14).Mode of...

Experimental evaluation of a spinning-mode acoustic-treatment design concept for aircraft inlets /

Heidelberg, Laurence J.
Homyak, Leonard.
Rice, Edward J.
Lewis Research Center.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Office.

January 1980

Apr. 1980."Lewis Research Center."Includes bibliographical references.Mode of access: Internet

Noise characteristics of jet flap type exhaust flows /

Schrecker, G. O.
Maus, J. R.
Langley Research Center.
University of Tennessee (System). Space Institute.

January 1974

"Prepared by the University of Tennessee Space Institute ... for Langley Research Center."Cover titl...

NASA research on noise-abatement approach profiles for multiengine jet transport aircraft /

Zalovcik, John A.
Schaefer, William T., Jr.
United States. National Aeronautics and Space Administration.
Langley Research Center.

January 1967

Work performed at Langley Research Center."June 1967."Includes bibliographical references (p. 14).Mo...

Numerical study of sound propagation in a jet flow /

Padula, Sharon L.
Liu, Chen-Huei.
Langley Research Center.

January 1975

Prepared at Langley Research Center.Cover title.Includes bibliographical references (p. 20).Mode of ...

A methodology for designing aircraft to low sonic boom constraints /

Mack, Robert J.
Needleman, Kathy E.
Langley Research Center.

January 1991

Prepared at Langley Research Center.Includes bibliographical references (p. 6).Mode of access: Inter...

Developmental design, fabrication, and test of acoustic suppressors for fans of high bypass turbofan engines /

Tucker, R. H.
Lewis Research Center.
Boeing Company. Wichita Division.

January 1974

"Prepared by the Boeing Company, Wichita, Kans. ... for Lewis Research Center."Cover title.Bibliogra...

Study and development of acoustic treatment for jet engine tailpipes /

Nelsen, M. D.
Langley Research Center.
Boeing Company. AVCO Corporation. Systems Division.
United States. National Aeronautics and Space Administration.

January 1971

Prepared by The Boeing Company for Langley Research Center.N72-10043.Includes bibliographical refere...

Cold-flow acoustic evaluation of a small-scale, divergent, lobed nozzle for supersonic jet noise suppression /

Huff, Ronald G.
Groesbeck, Donald E.
Lewis Research Center.

January 1975

Prepared at Lewis Research Center.Cover title.Includes bibliographical references (p. 23).Mode of ac...

Reduction of acoustic disturbances in the test section of supersonic wind tunnels by laminarizing their nozzle and test section wall boundary layers by means of suction /

Pfenninger, W.
Syberg, J.
Langley Research Center.
Boeing Commercial Airplane Company.

January 1974

"Prepared by Boeing Commercial Airplane Company ... for Langley Research Center."Cover title.Include...

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

Burley, Richard R.
Johns, Albert L.
Lewis Research Center.

January 1974

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

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...

Flight velocity effects on the jet noise of several variations of a 104-tube suppressor nozzle /

Burley, Richard R.
Lewis Research Center.

January 1974

Prepared at Lewis Research Center.Cover title.Includes bibliographical references (p. 23-24).Mode of...

Design of a bleed system for a Mach 3.5 inlet /

Syberg, J.
Hickcox, T. E.
Ames Research Center.
Boeing Company.

January 1973

"Prepared by the Boeing Company ... for Ames Research Center."Cover title.Bibliography: p. 32.Mode o...

Dispersion of turbojet engine exhaust in flight /

Holdeman, James D.
Lewis Research Center.

January 1973

Prepared at Lewis Research Center.Cover title.Includes bibliographical references (p. 15).Mode of ac...

Assessment of an analytical procedure for predicting supersonic ejector nozzle performance /

Anderson, Bernhard H.
Lewis Research Center.

January 1974

Prepared at Lewis Research Center.Cover title.Includes bibliographical references (p. 13-14).Mode of...

Experimental evaluation of a spinning-mode acoustic-treatment design concept for aircraft inlets /

Heidelberg, Laurence J.
Homyak, Leonard.
Rice, Edward J.
Lewis Research Center.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Office.

January 1980

Apr. 1980."Lewis Research Center."Includes bibliographical references.Mode of access: Internet

Noise characteristics of jet flap type exhaust flows /

Schrecker, G. O.
Maus, J. R.
Langley Research Center.
University of Tennessee (System). Space Institute.

January 1974

"Prepared by the University of Tennessee Space Institute ... for Langley Research Center."Cover titl...

NASA research on noise-abatement approach profiles for multiengine jet transport aircraft /

Zalovcik, John A.
Schaefer, William T., Jr.
United States. National Aeronautics and Space Administration.
Langley Research Center.

January 1967

Work performed at Langley Research Center."June 1967."Includes bibliographical references (p. 14).Mo...

Numerical study of sound propagation in a jet flow /

Padula, Sharon L.
Liu, Chen-Huei.
Langley Research Center.

January 1975

Prepared at Langley Research Center.Cover title.Includes bibliographical references (p. 20).Mode of ...

A methodology for designing aircraft to low sonic boom constraints /

Mack, Robert J.
Needleman, Kathy E.
Langley Research Center.

January 1991

Prepared at Langley Research Center.Includes bibliographical references (p. 6).Mode of access: Inter...

Development of acoustically lined ejector technology for multitube jet noise suppressor nozzles by model and engine tests over a wide range of jet pressure ratios and temperatures /

Abstract

Extracted data

Development of acoustically lined ejector technology for multitube jet noise suppressor nozzles by model and engine tests over a wide range of jet pressure ratios and temperatures /

Abstract

Extracted data

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