Compressible High Order Parallel Acoustics Solver

Award Information
Agency: Department of Defense
Branch: Navy
Contract: N68335-10-C-0407
Agency Tracking Number: N09A-008-0522
Amount: $749,735.00
Phase: Phase II
Program: STTR
Awards Year: 2010
Solicitation Year: 2009
Solicitation Topic Code: N09-T008
Solicitation Number: 2009.A
Small Business Information
PO Box 6971, Chesterfield, MO, 63006-
DUNS: 126752018
HUBZone Owned: N
Woman Owned: N
Socially and Economically Disadvantaged: N
Principal Investigator
 Philip Morris
 (814) 863-0157
Business Contact
 Alan Cain
Title: President
Phone: (314) 373-3311
Research Institution
 Penn State University
 Lisa Hipple
 110 Technology Center Bldg.
University Park, PA, 16802-
 (814) 863-4720
 Nonprofit college or university
The noise from turbulent, hot, supersonic jets during take-off and landing, as well as high-Mach cruise at altitude, dominates noise emanating from other powerplant components (e.g., fan, combustor). This intense noise has significant safety implications for launch personnel as well an environmental impact in the form of noise pollution around military installations. The proposed Phase II work will build on the successful Phase I effort to create a production CAA/CFD code which can accurately resolve the unsteady structures related to the dominant noise sources of high speed jets in realistic configurations. This software will predict the flow in and around realistic nozzle configurations and accurately capture the shock-containing jet plumes to enable physics-based noise predictions for these flows that include both jet mixing and shock-associated noise. The resulting software will enable the Navy customer to better design and engineer nozzle components and noise attenuation technologies for the low-bypass ratio powerplants of modern tactical aircraft.

* Information listed above is at the time of submission. *

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