SBIR/STTR Research Award
High-Speed Wind Tunnel Transient Dynamics During Start-up
Award amount
$149,993Program and phase
SBIR · Phase IAward year
2017Award details
- Awarding agency
- Department of Defense
- Branch
- Air Force
- Recipient company
- AHMIC AEROSPACE LLC
- Proposal award date
- 2017-09-13
- Contract end date
- 2018-06-13
- UEI
- YS94KQDW2HK9
- Solicitation number
- 2017.1
- Topic code
- AF171-019
Research abstract
Start and unstart conditions represent some of the worst possible aerodynamic loading scenarios a test article will experience in high-speed test facilities. Many facilities employ a model injection system to avoid such loading but must still account for
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.
- Dynamic Force Measurement Solution (DFMS) for Hypersonic Ground Testing
- Multidirectional Heat Flux Measurements from a Discrete Thermal Measurement Gauge
- Wall Shear Measurement Technology for Plume Surface Interactions
- Multi-directional Heat Flux Measurements from a Discrete Thermal Measurement Gage
- Efficient Ablation Modeling Framework using Triple Deck Theory and Machine Learning
Awards with the same topic code
Verified by an exact topic code match. This is not a text-similarity match.
- Flexible Software Toolset for Accurate Prediction of High-Speed Wind Tunnel Transient Airloads
- Flexible Software Toolset for Accurate Prediction of High-Speed Wind Tunnel Transient Airloads
Research funding history
16 SBIR/STTR records share this UEI (2015–2024). Reported award amounts total $7,637,317. Reported amounts are not federal obligations.
Phases: Phase I, Phase II, Phase II – Direct to Phase II
Agencies: Department of Defense, National Aeronautics and Space Administration