Prediction and Modal Analysis of Supersonic Jet Noise From Complex Nozzles in an Integrated Simulation Environment
Award amount
$124,733Program and phase
SBIR · Phase IAward year
2018Award details
- Awarding agency
- National Aeronautics and Space Administration
- Branch
- Not reported
- Recipient company
- CASCADE TECHNOLOGIES INC
- Proposal award date
- 2018-07-27
- Contract end date
- 2019-02-15
- UEI
- K9KCLNBFQAF6
- Solicitation number
- SBIR_18_P1
- Topic code
- A1
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.
- Tools and approaches for model-consistent data-enabled turbulence modeling for hypersonic flows
- GPU-accelerated LES framework for aeroacoustic predictions of integrated systems
- Software developments for large-eddy simulations on GPU-accelerated systems
- Mixed precision efficiency improvements for multi-physics flow simulations
- A GPU-Accelerated Full-Wheel Multi-Stage Turbomachinery Flow Solver
Research funding history
47 SBIR/STTR records share this UEI (2004–2022). Reported award amounts total $21,363,179. Reported amounts are not federal obligations.
Phases: Phase I, Phase II
Agencies: Department of Defense, National Aeronautics and Space Administration, Department of Energy