Aerodynamic Shape Optimization of a Blended-Wing-Body Aircraft
Author:
Affiliation:
1. University of Michigan, Ann Arbor
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.2013-283
Reference61 articles.
1. 50 years of transonic aircraft design
2. Guynn, M., Berton, J., Fisher, K., Haller, W., Tong, M., and Thurman, D. “Engine Concept Study for an Advanced Single-AisleTransport,”NASATM-2009-215784,2009.
3. The potential of turboprops for reducing aviation fuel consumption
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