Multifidelity Modeling of Deployable Wings: Multibody Dynamic Simulation and Wind Tunnel Experiment
Author:
Affiliation:
1. Tohoku University, Sendai 980-8579, Japan
2. University of Warwick, Coventry CV4 7AL, United Kingdom
3. Tohoku University, Sendai 980-8577, Japan
Funder
Institute of Fluid Science, Tohoku University
Japan Society for the Promotion of Science
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
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