Flow-Field Measurement of a Hybrid Wing Body Model with Blown Flaps
Author:
Affiliation:
1. NASA Langley Research Center
2. Northrop Grumman Corporation
3. Air Force Research Laboratory
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.2008-6718
Reference12 articles.
1. The Development of All–Wing Aircraft
2. Design of the Blended Wing Body Subsonic Transport
3. 5Guide for the Verification and Validation of Computational Fluid Dynamics Simulations, AIAA G-077-1998 (2002).
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