Hybrid Design for Aircraft Wind-Tunnel Testing Using Response Surface Methodologies
Author:
Affiliation:
1. Old Dominion University, Norfolk, Virginia 23529
2. Florida State University, Tallahassee, Florida 32310
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/1.25914
Reference14 articles.
1. Use of Designed Experiments in Wind Tunnel Testing of Performance Automobiles
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