Innovative Subgrid-Scale Combustion Modeling for Gas Turbines
Award amount
$99,499Program and phase
SBIR · Phase IAward year
2010Award details
- Awarding agency
- Department of Energy
- Branch
- Not reported
- Recipient company
- COMBUSTION RESEARCH & FLOW TECHNOLOGY INC
- Proposal award date
- Not reported
- Contract end date
- 2011-03-18
- UEI
- XGYZK5MHNJZ8
- Solicitation number
- DE-FOA-0000161
- Topic code
- 39 a
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.
- Innovative Subgrid-Scale Combustion Modeling for Gas Turbines
- Advanced Methods for Predicting 3D Unsteady Flows Around Wind Turbines
- Computational Particle Dynamic Simulations on Multicore Processors (CPDMu)
- Advanced Methods for Predicting 3D Unsteady Flows Around Wind Turbines
- Turbine Trailing Edge Noise Reduction Using Adjoint-Based Shape Optimization
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