SBIR/STTR Research Award
Advanced Flow Control Actuators for Fuselage Drag Reduction
Award amount
$119,700Program and phase
SBIR · Phase IAward year
2005Award details
- Awarding agency
- Department of Defense
- Branch
- Army
- Recipient company
- DOMZALSKI MACHINE
- Proposal award date
- 2004-12-09
- Contract end date
- 2005-06-09
- UEI
- Not reported
- Solicitation number
- 2004.3
- Topic code
- A04-082
Research abstract
The use of oscillatory jet active flow control offers the opportunity to dramatically reduce the parasitic drag of helicopter fueslages and their mission equipment without compromise of utility. A new class of actuator, flight qualification of actuators, and an integrated electronic driver and controller will make possible an efficient full-scale installation and flight test.
Technology keywords
Not reported
Awards with the same topic code
Verified by an exact topic code match. This is not a text-similarity match.
- Advanced Flow Control Actuators for Fuselage Drag Reduction
- Advanced Flow Control Actuators for Fuselage Drag Reduction
- Advanced Flow Control Actuators for Fuselage Drag Reduction