SBIR/STTR Research Award
FLOW FIELD SEPARATION APPROXIMATIONS FOR HYPERSONIC AERODYNAMICS
Award amount
$59,425Program and phase
SBIR · Phase IAward year
1987Award details
- Awarding agency
- Department of Defense
- Branch
- Air Force
- Recipient company
- GENERAL SCIENCES INC
- Proposal award date
- Not reported
- Contract end date
- Not reported
- UEI
- CSMXLC48L3V4
- Solicitation number
- Not reported
- Topic code
- Not reported
Research abstract
A STUDY IS PROPOSED TO DEVELOP MORE ACCURATE APPROXIMATE METHODS FOR PREDICTING FLOW SEPARATION PHENOMENA ON HYPERSONIC MANEUVERING AEROSPACE VEHICLES. EXPERIMENTAL DATA AND FLOW FIELD COMPUTATIONS WILL BE USED TO DERIVE IMPROVED SEMI-EMPIRICAL RELATIONS FOR INCIPIENT SEPARATION, SEPARATED REGION GEOMETRY, SURFACE PROPERTIES, AND FLOW FIELD PROFILES FROM SURFACE TO INVISCID EDGE OF THE SEPARATED REGION. THE MAJOR TYPES OF FLOW SEPARATION THAT WILL BE STUDIED INCLUDE LEESIDE, WINDWARD CONTROL SURFACES, AND SHOCK IMPINGEMENT ON ADJACENT SURFACES.
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.
- MIL-STD-1901A Compliant Igniter Energetic for Solid Rocket Motors
- Multifunctional Materials for Increased Lethality Munitions
- Hyper-Velocity Projectile (HVP) Warhead Optimization for Lethality
- MIL-STD-1901A Compliant Igniter Energetics for Solid Rocket Motors
- Novel Flame Inhibiting Materials to Increase Red Phosphorus Obscurant Safety
Research funding history
92 SBIR/STTR records share this UEI (1985–2021). Reported award amounts total $24,168,396. Reported amounts are not federal obligations.
Phases: Phase I, Phase II
Agencies: Department of Defense, National Aeronautics and Space Administration