Development of a Pendulum Support Rig Dynamic Wind Tunnel Apparatus
Author:
Affiliation:
1. University of Bristol
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.2002-4879
Reference11 articles.
1. Fourier functional analysis for unsteady aerodynamic modeling
2. State-space representation of aerodynamic characteristics of an aircraft at high angles of attack
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