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Modeling and Optimizing Turbines for Unsteady Flow
Award Information
Agency: Department of Defense
Branch: Defense Advanced Research Projects Agency
Contract: W911QX-13-C-0132
Agency Tracking Number: D13A-005-0026
Amount:
$99,998.00
Phase:
Phase I
Program:
STTR
Solicitation Topic Code:
ST13A-005
Solicitation Number:
2013.A
Timeline
Solicitation Year:
2013
Award Year:
2013
Award Start Date (Proposal Award Date):
2013-06-28
Award End Date (Contract End Date):
2013-12-31
Small Business Information
2629 Townsgate Road
Suite 105
Westlake Village, CA
-
United States
DUNS:
005100560
HUBZone Owned:
No
Woman Owned:
Yes
Socially and Economically Disadvantaged:
Yes
Principal Investigator
Name: Ramakanth Munipalli
Title: Sr. Computational Physicist
Phone: (805) 371-7500
Email: mrk@hypercomp.net
Title: Sr. Computational Physicist
Phone: (805) 371-7500
Email: mrk@hypercomp.net
Business Contact
Name: Vijaya Shankar
Title: Vice-President
Phone: (805) 371-7556
Email: vshankar@hypercomp.net
Title: Vice-President
Phone: (805) 371-7556
Email: vshankar@hypercomp.net
Research Institution
Name: University of Connecticut
Contact: Baki Cetegen
Address:
Phone: (860) 486-2966
Type: Nonprofit College or University
Contact: Baki Cetegen
Address:
191 Auditorium Road, Unit 3139
Storrs, CT
06269-3139
United States
Phone: (860) 486-2966
Type: 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. *
