Numerical Simulation of a Flexible X-Wing Flapping-Wing Micro Air Vehicle

Journal article (2017)

Authors

S. Deng Northwestern Polytechnical University
M. Perçin Aerodynamics - Aerospace Engineering
B.W. van Oudheusden Aerodynamics - Aerospace Engineering
H. Bijl Aerodynamics - Aerospace Engineering
T Xiao Nanjing University of Aeronautics and Astronautics
Research Group
Aerodynamics (Aerospace Engineering) (TU Delft)
Copyright: © 2017 S. Deng, M. Perçin, B.W. van Oudheusden, H. Bijl, B.D.W. Remes, T Xiao
DOI: https://doi.org/10.2514/1.J054816
More Info
expand_more

Published Date

2017

Language

English

Reuse Rights

Other than for strictly personal use, it is not permitted to download, forward or distribute the text or part of it, without the consent of the author(s) and/or copyright holder(s), unless the work is under an open content license such as Creative Commons.

Faculty

Aerospace Engineering

Department

Flow Physics and Technology

Research Group

Aerodynamics

Files

AIAA_Journal_2017_Deng_R2.pdf
(pdf | 2.54 Mb)
- Embargo expired in 01-07-2018