Rule-Based Multidisciplinary Tool for Unsteady Reacting Real-Fluid Flows
Award amount
$599,926Program and phase
SBIR · Phase IIAward year
2005Award details
- Awarding agency
- National Aeronautics and Space Administration
- Branch
- Not reported
- Recipient company
- STREAMLINE NUMERICS, INC.
- Proposal award date
- 2004-11-22
- Contract end date
- 2006-11-22
- UEI
- YSLNMSL67YC7
- Solicitation number
- Not reported
- Topic code
- A4.06
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.
- Computationally Efficient Multiphase Flow Simulation Tool for Propulsion Test Technology Components
- Multiphase Hypergolic Combustion Simulation Tool Based on Algebraic VOF and Compressible Flamelet Methodologies
- A Fast and Robust PIMPLE-Based Algebraic VOF Method for Two-Phase Compressible Flows
- High Performance Solver for Coupled Cavitation and Fluid-Structure Interaction in Cryogenic Environments
- Multiphysics Modeling of Dynamic Combustion Processes Using Pareto-Efficient Combustion Framework
Awards with the same topic code
Verified by an exact topic code match. This is not a text-similarity match.
- Low-Mass VOST Valve
- Modeling Unsteady Cavitation Effects and Dynamic Loads in Cryogenic Systems
- Rule-Based Multidisciplinary Tool for Unsteady Reacting Real-Fluid Flows
- Modeling Unsteady Cavitation Effects and Dynamic Loads in Cryogenic Systems
- Low-Mass VOST Valve
Research funding history
32 SBIR/STTR records share this UEI (2004–2022). Reported award amounts total $11,051,944. Reported amounts are not federal obligations.
Phases: Phase I, Phase II
Agencies: National Aeronautics and Space Administration, Department of Defense