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Dynamics / Jet noise / Combustion chamber / Combustion / Rocket engine / Turbojet / Gas turbine / Turbofan / Engine / Jet engines / Fluid dynamics / Fluid mechanics


Aeroacoustics I. Duran (Cerfacs, Snecma) S. Moreau (Universite de Sherbrooke)
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Document Date: 2014-06-18 08:46:19

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Company

Modern Aero / /

Country

United States / /

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Facility

Stanford University / German Aerospace Center / /

IndustryTerm

acoustic energy / electrical heating device / signal post-processing / noise reduction technologies / analytical solutions / gas constant / hot combustion products / numerical solution / /

NaturalFeature

Inlet Mach / SINAI / /

Organization

Institut de Mecanique / Center for Turbulence Research / American Rocket Society / Stanford University / European Commission / National Aeronautics and Space Administration / Acoustical Society of America / Universite Montpellier / Universite de Sherbrooke / German Aerospace Center / /

Person

Eddy Model / Friedrich Bake / Proc / Reynolds-Averaged Navier-Stokes / E. Bouty / Nancy Kings / /

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Position

editor / T.-D. BUTLER / /

Product

Olympus W-10 Voice Recorder / /

ProvinceOrState

Colorado / /

PublishedMedium

Journal of Sound and Vibration / Journal of Fluid Mechanics / /

SportsLeague

Stanford University / /

Technology

radiation / broadband / DNS / noise reduction technologies / aero / http / simulation / /

URL

http /

SocialTag