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

Transonic performance characteristics of several jet noise suppressors /

Schmeer, James W.
Cassetti, Marlowe D.
Salters, Leland B.
United States. National Aeronautics and Space Administration.

Cover title."July 1960."Aircraft; Aircraft safety and noise; Propulsion system elements.Includes bib...

Combustion contribution to noise in jet engines /

Plett, E. G.
United States. National Aeronautics and Space Administration.
Langley Research Center.
Princeton University.

January 1976

Cover title.Includes bibliographical references (p. 24-25).Mode of access: Internet

Effect of treated length on performance of full-scale turbofan inlet noise suppressors /

Dittmar, James H.
Groeneweg, John F. (John Frederick), 1937-
Lewis Research Center.

January 1974

Prepared at Lewis Research Center.Cover title.Includes bibliographical references (p. 14-15).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 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...

Low-speed jet noise from a 1.83-meter (6-ft) fan for tubrofan engines /

Minner, Gene L. (Gene Logan), 1942-
Feiler, Charles E.
United States. National Aeronautics and Space Administration.
Lewis Research Center.

January 1971

Prepared at Lewis Research Center.Cover title.Includes bibliographical references (p. 8-9).Mode of a...

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...

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...

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...

Flight Reynolds number effects on a contoured boattail nozzle at subsonic speeds /

Chamberlin, Roger.
Lewis Research Center.

January 1974

Prepared at Lewis Research Center.Cover title.Includes bibliographical references (p. 8-9).Mode of a...

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 ...

Effects of temperature on noise of bypass jets as measured in the Langley noise research facility /

Kantarges, George T.
Cawthorn, Jimmy M.
United States. National Aeronautics and Space Administration.
Langley Research Center.

"August 1964"--Cover.Includes bibliographical references.Mode of access: Internet

An analytical study of the effects of jets located more than one jet diameter above a wing at subsonic speeds /

Putnam, Lawrence E. (Lawrence Elwood)
Langley Research Center.

January 1974

Prepared at Langley Research Center.Cover title.Includes bibliographical references (p. 12-13).Mode ...

Acoustic, performance, and wake survey measurements of a lobed velocity-decayer nozzle installed on a quieted TF-34 turbofan engine /

Samanich, Nick E.
Heidelberg, Laurence J.
United States. National Aeronautics and Space Administration.
Lewis Research Center.

January 1976

Cover title.Includes bibliographical references (p. 15-16).Mode of access: Internet

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 /

Atvars, J.
Lewis Research Center.
Boeing Commercial Airplane Company.

January 1974

"Prepared by Boeing Commercial Airplane Company ... for Lewis Research Center."Cover title.Includes ...

Transonic performance characteristics of several jet noise suppressors /

Schmeer, James W.
Cassetti, Marlowe D.
Salters, Leland B.
United States. National Aeronautics and Space Administration.

Cover title."July 1960."Aircraft; Aircraft safety and noise; Propulsion system elements.Includes bib...

Combustion contribution to noise in jet engines /

Plett, E. G.
United States. National Aeronautics and Space Administration.
Langley Research Center.
Princeton University.

January 1976

Cover title.Includes bibliographical references (p. 24-25).Mode of access: Internet

Effect of treated length on performance of full-scale turbofan inlet noise suppressors /

Dittmar, James H.
Groeneweg, John F. (John Frederick), 1937-
Lewis Research Center.

January 1974

Prepared at Lewis Research Center.Cover title.Includes bibliographical references (p. 14-15).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 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...

Low-speed jet noise from a 1.83-meter (6-ft) fan for tubrofan engines /

Minner, Gene L. (Gene Logan), 1942-
Feiler, Charles E.
United States. National Aeronautics and Space Administration.
Lewis Research Center.

January 1971

Prepared at Lewis Research Center.Cover title.Includes bibliographical references (p. 8-9).Mode of a...

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...

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...

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...

Flight Reynolds number effects on a contoured boattail nozzle at subsonic speeds /

Chamberlin, Roger.
Lewis Research Center.

January 1974

Prepared at Lewis Research Center.Cover title.Includes bibliographical references (p. 8-9).Mode of a...

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 ...

Effects of temperature on noise of bypass jets as measured in the Langley noise research facility /

Kantarges, George T.
Cawthorn, Jimmy M.
United States. National Aeronautics and Space Administration.
Langley Research Center.

"August 1964"--Cover.Includes bibliographical references.Mode of access: Internet

An analytical study of the effects of jets located more than one jet diameter above a wing at subsonic speeds /

Putnam, Lawrence E. (Lawrence Elwood)
Langley Research Center.

January 1974

Prepared at Langley Research Center.Cover title.Includes bibliographical references (p. 12-13).Mode ...

Acoustic, performance, and wake survey measurements of a lobed velocity-decayer nozzle installed on a quieted TF-34 turbofan engine /

Samanich, Nick E.
Heidelberg, Laurence J.
United States. National Aeronautics and Space Administration.
Lewis Research Center.

January 1976

Cover title.Includes bibliographical references (p. 15-16).Mode of access: Internet

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 /

Atvars, J.
Lewis Research Center.
Boeing Commercial Airplane Company.

January 1974

"Prepared by Boeing Commercial Airplane Company ... for Lewis Research Center."Cover title.Includes ...

Transonic performance characteristics of several jet noise suppressors /

Schmeer, James W.
Cassetti, Marlowe D.
Salters, Leland B.
United States. National Aeronautics and Space Administration.

Cover title."July 1960."Aircraft; Aircraft safety and noise; Propulsion system elements.Includes bib...

Combustion contribution to noise in jet engines /

Plett, E. G.
United States. National Aeronautics and Space Administration.
Langley Research Center.
Princeton University.

January 1976

Cover title.Includes bibliographical references (p. 24-25).Mode of access: Internet

Effect of treated length on performance of full-scale turbofan inlet noise suppressors /

Dittmar, James H.
Groeneweg, John F. (John Frederick), 1937-
Lewis Research Center.

January 1974

Prepared at Lewis Research Center.Cover title.Includes bibliographical references (p. 14-15).Mode of...

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

Abstract

Extracted data

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

Abstract

Extracted data

Related items

Related items