Document Type
Article
Journal/Book Title/Conference
College of Engineering Senior Design Projects
Publisher
Utah State University
Publication Date
2019
Abstract
Wing dimpling due to hail damage can result in costly aircraft reskin efforts
Objective: Determine the aerodynamic effects of hail damage on a NACA 0012 wing section
- Angle where the aircraft stalls
- The maximum lift of the aircraft
- The drag on the aircraft due to dimpling
Recommended Citation
Crapo, Allen; Krebs, Dallin; and Miller, Janelle, "Hail Damage Test Process Design USAF" (2019). Mechanical and Aerospace Engineering. Paper 9.
https://digitalcommons.usu.edu/maeengr_srdesign/9