Numerical calculation of unsteady transonic potential flow over three-dimensional wings with oscillating control surfaces
Author:
Affiliation:
1. National Aerospace Laboratory, Tokyo, Japan
2. FACOM-HITAC Inc., Tokyo, Japan
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/3.8425
Reference23 articles.
1. Unsteady Subsonic Aerodynamic Loadings Caused by Control Surface Motions
2. Numerical Solution of Three-Dimensional Unsteady Transonic Flow over Swept Wings
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