Rapid Technology Focused Experimental and Computational Aerodynamic Investigation of a Strike Tanker
Author:
Affiliation:
1. Air Force Research Laboratory
2. Air Force Institute of Technology
3. University of Dayton Research Institute
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.2004-6870
Reference7 articles.
1. Tyler, C., Braisted, W., Higgins, J. "Evaluation of Rapid Prototyping Technologies for Use in Wind Tunnel Model Fabrication," AIAAPaper2005-1301.
2. Liebeck, R.H. "Blended Wing Body Design Challenges",AIAAPaper2003-2659.
3. Design of the Blended Wing Body Subsonic Transport
4. Stall Resistance Features of Lifting-Body Airplane Configurations
5. Design and Testing of a Blended Wing Body Aeroelastic Wind-Tunnel Model
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