Reduced-Order Kinetic Models for Real Fuels Applicable to High-Pressure Turbulent Flows
Award amount
$149,996Program and phase
STTR · Phase IAward year
2016Award details
- Awarding agency
- Department of Defense
- Branch
- Army
- Recipient company
- COMBUSTION RESEARCH & FLOW TECHNOLOGY INC
- Proposal award date
- 2016-08-16
- Contract end date
- 2017-04-15
- UEI
- XGYZK5MHNJZ8
- Solicitation number
- 2016.0
- Topic code
- A16A-T001
Research abstract
Technology keywords
Not reported
Other awards by this recipient
Verified by the same UEI. These are other public SBIR/STTR award pages, not a merged company record.
- Predicting RF Attenuation and Radar Cross Section Returns for High Fidelity 3D Missile Plumes and Hypersonic Wakes with Hardbody Interaction
- Efficient Models for Film Condensation in Cryogenic Tank Applications
- Framework for Transitioning DTRA High Fidelity Codes to APUs
- Landing Area and Rocket Plume Diagnostics
- A Multi-Zonal Multi-Timescale Modeling Framework to Accelerate Fluid-Thermal Analyses of Rotating Detonation Rocket Engines
Awards with the same topic code
Verified by an exact topic code match. This is not a text-similarity match.
- Using the Conditional Moment Closure Method to Assess the Effects of Turbulence Chemical Kinetics
- Chemical Kinetic Pathway Effects in Turbulent Reacting Flows
- Using the Conditional Moment Closure Method to Assess the Effects of Turbulence Chemical Kinetics
Research funding history
303 SBIR/STTR records share this UEI (1995–2025). Reported award amounts total $121,181,328. Reported amounts are not federal obligations.
Phases: Phase I, Phase II, Phase II – Direct to Phase II
Agencies: Department of Defense, National Aeronautics and Space Administration, Department of Energy, National Science Foundation