Hybrid Wing Body Performance Validation at the National Transonic Facility
Author:
Affiliation:
1. Lockheed Martin Corporation
2. NASA Langley Research Center
3. Air Force Research Laboratory
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.2017-0099
Reference10 articles.
1. Hooker, J.R., Wick, A.T. "Design and the Hybrid Wing Body for Fuel Efficient Air Mobility Operations," AIAA-2014-1285.
2. Over Wing Nacelle Installations for Improved Energy Efficiency
3. Hooker, J.R., Wick, A.T., Zeune, C., Jones, G., and Milholen, W. "Design and Transonic Wind Tunnel Testing of a Cruise Efficient STOL Military Transport," AIAA-2013-1100.
4. Assessment of an unstructured-grid method for predicting 3-D turbulent viscous flows
5. Campbell, R.L. "Efficient Viscous Design of Realistic Aircraft Configurations," AIAA 1998-2539
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