Conceptual Design and Structural Analysis of an Open Rotor Hybrid Wing Body Aircraft
Author:
Affiliation:
1. NASA Langley Research Center
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.2013-1688
Reference19 articles.
1. Design of the Blended-Wing-Body subsonic transport
2. Risch, T., Cosentino, G., Regan, C.D., Kisska, M., and Princen, N. "X-48B Flight-Test Progress Overview," AIAA-2009-0934,47thAIAAAerospaceSciencesMeetingandExhibit,January5-8,2009,Orlando,Florida.
3. Finite Element Based HWB Centerbody Structural Optimization and Weight Prediction
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