SBIR/STTR Research Award
CFD Fuel Injector Design Tool Applicable To High-Pressure Vitiated Augmentor Flow
Award amount
$649,995Program and phase
SBIR · Phase IIAward year
2005Award details
- Awarding agency
- Department of Defense
- Branch
- Air Force
- Recipient company
- Flow Parametrics, LLC
- Proposal award date
- 2005-09-13
- Contract end date
- 2007-09-14
- UEI
- Not reported
- Solicitation number
- 2004.1
- Topic code
- AF04-293
Research abstract
Liquid fuel injection into heated and vitiated cross flows, at elevated pressures, will be investigated experimentally and through numerical simulations. Experimental efforts will include advanced optical measurements of liquid spray parameters at positions close to the injection site, as well as downstream. Liquid spray modeling will include first-principles, physics-bsaed modeling of liquid breakup and atomization, coupled with a Navier-Stokes flow solver equipped with advanced aerodynamics, droplet tracking, evaporation, and chemical kinetics models. The results will be useful to AFRL, AEDC and the US gas turbine industry in providing a validated simulation code applicable to military turbine augmentors, with the validation performed at operating conditions similare to actual augmentor conditions.
Technology keywords
Not reported
Awards with the same topic code
Verified by an exact topic code match. This is not a text-similarity match.
- CFD Fuel Injector Design Tool Featuring Unsteady Atomization and Turbulent-Combustion Models
- CFD Fuel Injector Design Tool Featuring Unsteady Atomization and Turbulent-Combustion Models
- CFD Design Tool for Fuel Injectors in Turbine Engines