Evaluation of a Three Degree of Freedom Test Rig for Stability Derivative Estimation
Author:
Affiliation:
1. University of Bristol, Bristol, BS8 1TR England, United Kingdom
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/1.19821
Reference35 articles.
1. Applications of Computational Methods for Dynamic Stability and Control Derivatives
2. Simulation of Flow About Rotating Forebodies at High Angles of Attack
3. Experimental Validation of the Wing Dihedral Effect Using a Whirling Arm Equipment
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