Design and Test of an Active Pneumatic Trailing Edge Flap for High-Speed Rotorcraft
F-0078-2022-17488
5/10/2022
- Content
- ABSTRACT
- Pages
- 11
- Citation
- DiPalma, M., Conti, ., Matalanis, ., Bates, P., et al., "Design and Test of an Active Pneumatic Trailing Edge Flap for High-Speed Rotorcraft," Vertical Flight Society 78th Annual Forum and Technology Display, Fort Worth, Texas, May 10, 2022, .