Structural Analysis and Testing of an Ultralight Unmanned-Aerial-Vehicle Carbon-Composite Wing
Author:
Affiliation:
1. Mississippi State University, Mississippi State, Mississippi 39762
2. Spirit AeroSystems, Wichita, Kansas 67278
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/1.36415
Reference8 articles.
1. Design of the Air Force Research Laboratory Micro Aerial Vehicle Research Configuration
2. Design of an Unmanned Aerial Vehicle for Ecological Conservation
3. AIRCRAFT AIRWORTHINESS CERTIFICATION: STATIC BENCH TESTING OF AN AIRFOIL ELEVATOR
4. Static test of an ultralight airplane
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