SBIR/STTR Research Award
Miniaturized Parametric Inlet Bleed Module with Integrated Discretized Flow Control
Award amount
$874,989Program and phase
SBIR · Phase IIAward year
2017Award details
- Awarding agency
- Department of Defense
- Branch
- Air Force
- Recipient company
- Innoveering, LLC
- Proposal award date
- 2016-10-21
- Contract end date
- 2020-05-29
- UEI
- UGWNU2AMKF63
- Solicitation number
- 15.1
- Topic code
- AF151-188
Research abstract
The interaction of high Mach flows with the aircraft and engine structures generates complex fluid dynamic phenomena that include shock waves, shear layers, vortices, and separated flows, all of which can be further influenced by the thermochemical behavi
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.
- Autonomous Flight Safety System for Submarine Launch (AFSS-SUB)
- Advanced Hypersonic Engine Manufacturing System
- S1X3000 Scramjet for Air-Launched Responsive Strike Missile (ARSM): Freejet Test Article for a Compact Scramjet Engine
- Novel Fluidic Flow Control of Scramjet Isolators
- MEMS Solid State Semiconductor based Thermionic Converter (“mSSTiC”)
Awards with the same topic code
Verified by an exact topic code match. This is not a text-similarity match.
- Innovative Methods for Parametric Bleed Pattern Variation in Wind Tunnel Models
- Miniaturized parametric inlet bleed module with integrated discretized flow control
- Innovative Methods for Parametric Bleed Pattern Variation in Wind Tunnel Models
Research funding history
40 SBIR/STTR records share this UEI (2015–2022). Reported award amounts total $23,063,825. Reported amounts are not federal obligations.
Phases: Phase I, Phase II, Phase II – Direct to Phase II
Agencies: Department of Defense, Department of Commerce, National Aeronautics and Space Administration, Department of Energy