Aeroacoustics of Contoured and Solid Porous Conical Plug Nozzle Supersonic Jet Flows

Aeroacoustics of Contoured and Solid Porous Conical Plug Nozzle Supersonic Jet Flows PDF Author:
Publisher:
ISBN:
Category : Jets
Languages : en
Pages :

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Aeroacoustics of Contoured and Solid Porous Conical Plug Nozzle Supersonic Jet Flows

Aeroacoustics of Contoured and Solid Porous Conical Plug Nozzle Supersonic Jet Flows PDF Author:
Publisher:
ISBN:
Category : Jets
Languages : en
Pages :

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Aeroacoustics of Supersonic Jet Flows from Contoured and Solid/porous Conical Plug-nozzles

Aeroacoustics of Supersonic Jet Flows from Contoured and Solid/porous Conical Plug-nozzles PDF Author:
Publisher:
ISBN:
Category :
Languages : en
Pages : 192

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Aeroacoustics of Supersonic Jet Flows from Contoured and Solid-porous Conical

Aeroacoustics of Supersonic Jet Flows from Contoured and Solid-porous Conical PDF Author:
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Category :
Languages : en
Pages :

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Computational Study of a Contoured Plug-nozzle as a Supersonic Jet Noise Suppressor

Computational Study of a Contoured Plug-nozzle as a Supersonic Jet Noise Suppressor PDF Author:
Publisher:
ISBN:
Category :
Languages : en
Pages : 84

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Scientific and Technical Aerospace Reports

Scientific and Technical Aerospace Reports PDF Author:
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 1126

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Lists citations with abstracts for aerospace related reports obtained from world wide sources and announces documents that have recently been entered into the NASA Scientific and Technical Information Database.

Computational Noise Study of a Supersonic Short Conical Plug-Nozzle Jet

Computational Noise Study of a Supersonic Short Conical Plug-Nozzle Jet PDF Author: National Aeronautics and Space Administration (NASA)
Publisher: Createspace Independent Publishing Platform
ISBN: 9781722313289
Category :
Languages : en
Pages : 86

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A computational jet noise study of a short conical plug-nozzle (CPN) is presented. The CPN has an exit diameter of 45 mm and the geometrical configuration closely approximates that of an ideal contoured plug-nozzle having shockless flow at pressure ratio xi(sub d) = 3.62. The gasdynamics of the jet flows have been predicted using the CFD code, NPARC with k-epsilon turbulence model; these data are then used for noise computations based on the modified GE/MGB code. The study covers a range of pressure ratio, 2.0 less than or equal to xi less than or equal to 5.0. The agreement of the computational results with the available experimental data is favorable. The results indicate consistent noise reduction effectiveness of the CPN as compared to equivalent convergent, convergent-divergent and ideal contoured plug nozzles at all pressure ratios. At design pressure ratio, codes predict noise levels within 4.0 dB of the measurements; and at off-design pressure ratios, in general, within 5.0 dB except at very high frequencies when deviations up to 10 dB are noted. The shock formation mechanism in the CPN jet is noted to be basically different from those in the convergent and CD nozzle jets. Das, Indu S. and Khavaran, Abbas and Das, A. P. Glenn Research Center...

Monthly Catalog of United States Government Publications

Monthly Catalog of United States Government Publications PDF Author:
Publisher:
ISBN:
Category : Government publications
Languages : en
Pages : 1092

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Government Reports Annual Index

Government Reports Annual Index PDF Author:
Publisher:
ISBN:
Category : Government reports announcements & index
Languages : en
Pages : 954

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Monthly Catalogue, United States Public Documents

Monthly Catalogue, United States Public Documents PDF Author:
Publisher:
ISBN:
Category : Government publications
Languages : en
Pages : 1094

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Government Reports Announcements & Index

Government Reports Announcements & Index PDF Author:
Publisher:
ISBN:
Category : Science
Languages : en
Pages : 1276

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