Efficient Methods for Complex Aircraft Configuration Aerodynamic Characterization using Response Surface Methodologies
Author:
Affiliation:
1. Old Dominion University
2. Florida State University
3. NASA Langley Research Center
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.2006-922
Reference18 articles.
1. Blended-Wing-Body Technology Study," Final Report, NASA Contract NAS1-20275, Boeing Report CRAD-9405-TR-3780,Oct.1997.
2. Design of the Blended-Wing-Body subsonic transport
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