Plasma Flow Control for Drag Reduction
Award amount
$124,859Program and phase
SBIR · Phase IAward year
2015Award details
- Awarding agency
- National Aeronautics and Space Administration
- Branch
- Not reported
- Recipient company
- INNOVATIVE TECH APPLICATIONS LLC
- Proposal award date
- 2015-06-17
- Contract end date
- 2015-12-17
- UEI
- ENJSTAA9R2V5
- Solicitation number
- Not reported
- Topic code
- A1.02
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
- Reduced-Order Model for the Prediction of Supersonic Aircraft Jet Noise
- Adjoint-Based Shape Optimization for Noise Reduction
- Plasma Fairings for Quieting Aircraft Landing Gear Noise
Awards with the same topic code
Verified by an exact topic code match. This is not a text-similarity match.
- Continuous-Scan Phased Array Measurement Methods for Turbofan Engine Acoustic Testing
- High Channel Count, High Density Microphone Arrays for Wind Tunnel Environments
- High Fidelity Tool for Noise Source Identification
- Continuous-Scan Phased Array Measurement Methods for Turbofan Engine Acoustic Testing
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