Modeling and Optimizing Turbines for Unsteady Flow

Award Information
Agency:
Department of Defense
Branch
Defense Advanced Research Projects Agency
Amount:
$99,950.00
Award Year:
2013
Program:
STTR
Phase:
Phase I
Contract:
W911QX-13-C-0131
Award Id:
n/a
Agency Tracking Number:
D13A-005-0006
Solicitation Year:
2013
Solicitation Topic Code:
ST13A-005
Solicitation Number:
2013.A
Small Business Information
1701 Military Trail, Suite 110, Jupiter, FL, -
Hubzone Owned:
N
Minority Owned:
N
Woman Owned:
Y
Duns:
048159342
Principal Investigator:
Frank Huber
Program Manager
(561) 427-6245
FHuber@fttinc.com
Business Contact:
Lloyd Mazer
Director of Contracts and Pricing
(561) 427-6337
LMazer@fttinc.com
Research Institute:
University of Florida
Corin Segal
PO BOX 116250
Gainesville, FL, 32611-6250
(352) 392-6132
Nonprofit college or university
Abstract
Pressure gain combustion has the potential to significantly improve the specific fuel consumption for gas turbine engines by realizing a pressure rise through the combustor as opposed to a pressure drop. One drawback to this form of combustion is the cycl

* information listed above is at the time of submission.

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