Advanced Physics Modeling for Gas Turbine Particulate Ingestion
Award amount
$1,000,000Program and phase
STTR · Phase IIAward year
2024Award details
- Awarding agency
- Department of Defense
- Branch
- Navy
- Recipient company
- COMBUSTION RESEARCH & FLOW TECHNOLOGY INC
- Proposal award date
- 2024-04-23
- Contract end date
- 2026-11-01
- UEI
- XGYZK5MHNJZ8
- Solicitation number
- 23.A
- Topic code
- N23A-T003
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.
- Advanced Physics Modeling for Gas Turbine Particulate Ingestion
- Improved Physics Modeling for Sand Particulate Tracking and Deposition in Gas Turbine Engines
- Improved Particle Tracking Through Efficient Scale-Resolving Simulations and Advance Physics Models
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