About this scholarly article

24th AIAA Applied Aerodynamics Conference - Low Reynolds Number High-Lift Airfoil Design for HALE Concept UAV by Liu, Qiang; Li, Jie; Zhou, Zhou is a scholarly article available to read on EtoBox.

Author

Liu, Qiang; Li, Jie; Zhou, Zhou

Publisher

American Institute of Aeronautics and Astronautics

Published

2006

Language

EN