Computational Modeling of Propeller Noise: NASA SR-7A propeller

dc.contributor.author	Moussa, Karim
dc.date.accessioned	2014-05-14 18:28:24 (GMT)
dc.date.available	2014-05-14 18:28:24 (GMT)
dc.date.issued	2014-05-14
dc.date.submitted	2014
dc.identifier.uri	http://hdl.handle.net/10012/8446
dc.description.abstract	The aerospace industry has been concerned with propeller noise levels for years. This interest is two-fold: government regulation and comfort in cabin. This report attempts to create a simulation mechanism needed to evaluate the far-field noise generation levels. However, in order to do that, the tandem cylinder case was evaluated first as a validation step before the SR-7A propeller case was performed. Both cases use STAR-CCM+, a commercial software, to perform the simulations.	en
dc.language.iso	en	en
dc.publisher	University of Waterloo	en
dc.subject	NASA	en
dc.subject	SR-7A	en
dc.subject	Aeroacoustics	en
dc.subject	Sound Pressure Level	en
dc.subject	Aerodynamics	en
dc.subject	Tandem cylinder	en
dc.subject	Detached Eddy Simulation	en
dc.subject	Turbulence modeling	en
dc.subject	Fluid mechanics	en
dc.subject	k-omega SST	en
dc.subject	Unsteady Pressure coefficient	en
dc.subject	Sound directivity	en
dc.title	Computational Modeling of Propeller Noise: NASA SR-7A propeller	en
dc.type	Master Thesis	en
dc.pending	false
dc.subject.program	Mechanical Engineering	en
uws-etd.degree.department	Mechanical and Mechatronics Engineering	en
uws-etd.degree	Master of Science	en
uws.typeOfResource	Text	en
uws.peerReviewStatus	Unreviewed	en
uws.scholarLevel	Graduate	en