Modeling and Optimizing Turbines for Unsteady Flow

Award Information
Agency:
Department of Defense
Branch
Defense Advanced Research Projects Agency
Amount:
$99,998.00
Award Year:
2013
Program:
STTR
Phase:
Phase I
Contract:
W911QX-13-C-0132
Award Id:
n/a
Agency Tracking Number:
D13A-005-0026
Solicitation Year:
2013
Solicitation Topic Code:
ST13A-005
Solicitation Number:
2013.A
Small Business Information
2629 Townsgate Road, Suite 105, Westlake Village, CA, -
Hubzone Owned:
N
Minority Owned:
Y
Woman Owned:
Y
Duns:
005100560
Principal Investigator:
Ramakanth Munipalli
Sr. Computational Physicist
(805) 371-7500
mrk@hypercomp.net
Business Contact:
Vijaya Shankar
Vice-President
(805) 371-7556
vshankar@hypercomp.net
Research Institute:
University of Connecticut
Baki Cetegen
191 Auditorium Road, Unit 3139
Storrs, CT, 06269-3139
(860) 486-2966
Nonprofit college or university
Abstract
Pressure gain combustion (PGC) offers means to a more efficient energy use in propulsion and power generation devices. Integrating PGC concepts in gas turbine engines often results in highly unsteady flow conditions at turbine inlet. Further, the backpres

* information listed above is at the time of submission.

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