Active Flow Control with Adaptive Design Techniques for Improved Aircraft Safety

Period of Performance: 01/01/2008 - 12/31/2008


Phase 2 STTR

Recipient Firm

Barron Assoc., Inc.
Firm POC
Principal Investigator

Research Institution

University of Virginia
351 McCormick Rd ECE Dept., Thornton Hall
Charlottesville, VA 22904


The overall objective of this STTR effort is to evaluate and demonstrate the potential for well-designed, strategically-located synthetic jet actuators to provide improved aircraft safety by: (1) delaying wing stall and improving aircraft controllability at high angles of attack and (2) providing low-cost actuation redun-dancy to improve controllability in the event of a mechanical control surface failure. Delaying flow separa-tion (i.e., wing stall) and providing "back-up" control power could allow an aircraft to recover from adverse conditions (due to a control surface failure, pilot/autopilot error, etc.) that would otherwise result in a loss of control.