Design and Test of an Active Pneumatic Trailing Edge Flap for High-Speed Rotorcraft

F-0078-2022-17488

5/10/2022

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Abstract
Content
ABSTRACT

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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, .
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Publisher
Published
5/10/2022
Product Code
F-0078-2022-17488
Content Type
Technical Paper
Language
English