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
Awards Year: 2013
Solicitation Year: 2013
Solicitation Topic Code: ST13A-005
Solicitation Number: 2013.A
Small Business Information
2629 Townsgate Road, Suite 105, Westlake Village, CA, -
DUNS: 005100560
HUBZone Owned: N
Woman Owned: Y
Socially and Economically Disadvantaged: Y
Principal Investigator
 Ramakanth Munipalli
 Sr. Computational Physicist
 (805) 371-7500
 mrk@hypercomp.net
Business Contact
 Vijaya Shankar
Title: Vice-President
Phone: (805) 371-7556
Email: vshankar@hypercomp.net
Research Institution
 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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