Localized High Fidelity Aeroacoustics Simulations of High Speed Impinging Jets in Operational Conditions
Award amount
$79,997Program and phase
SBIR · Phase IAward year
2010Award details
- Awarding agency
- Department of Defense
- Branch
- Navy
- Recipient company
- INNOVATIVE TECH APPLICATIONS LLC
- Proposal award date
- 2010-09-23
- Contract end date
- 2011-03-23
- UEI
- ENJSTAA9R2V5
- Solicitation number
- 2010.2
- Topic code
- N102-133
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.
- Plasma Actuation for Turbulent Skin Friction Drag Reduction on Wing Sections
- Plasma Flow Control for Drag Reduction
- Plasma Flow Control for Drag Reduction
- Reduced-Order Model for the Prediction of Supersonic Aircraft Jet Noise
- Adjoint-Based Shape Optimization for Noise Reduction
Awards with the same topic code
Verified by an exact topic code match. This is not a text-similarity match.
- Aeroacoustics of High-Speed Jet Impingement
- Aeroacoustics of High-Speed Jet Impingement
- Adaptive, Overset-Mesh Methodology for the Aeroacoustic Prediction of High-Speed Impinging Jets Using Large-Eddy Simulation
- Aeroacoustics of High-Speed Jet Impingement
Research funding history
33 SBIR/STTR records share this UEI (2000–2017). Reported award amounts total $9,590,194. Reported amounts are not federal obligations.
Phases: Phase I, Phase II
Agencies: Department of Defense, National Aeronautics and Space Administration