The Adaptive Compliant Trailing Edge (ACTE) flap was flown on the NASA Gulfstream GIII test bed at the NASA Armstrong Flight Research Center. This smoothly curving flap replaced the existing Fowler flaps creating a seamless control surface. This compliant structure, developed by FlexSys Inc. in partnership with Air Force Research Laboratory, supported NASA objectives for airframe structural noise reduction, aerodynamic efficiency, and wing weight reduction through gust load alleviation. A thorough structures airworthiness approach was developed to move this project safely to flight.
Approach for Structurally Clearing an Adaptive Compliant Trailing Edge Flap for Flight
2015
20 pages
Report
No indication
English
Civil Engineering , Quality Control & Reliability , Test Facilities & Equipment , Air Transportation , Aircraft , Checkout , Trailing edge flaps , Aircraft maintenance , Certification , Adaptive control , Procedures , Modulus of elasticity , Dynamic structural analysis , Structural health monitoring , Inspection , Quality control , Research aircraft , Flight test vehicles , Ground tests , Load tests , Flight tests , Elastic deformation , Twisting
Adaptive Compliant Trailing Edge (ACTE) Flight Testing
NTRS | 2018
|Adaptive Compliant Trailing Edge (ACTE) Flight Testing
NTIS | 2018
|