Powered Low Speed Testing of the Hybrid Wing Body
Author:
Affiliation:
1. Lockheed Martin Corporation
2. Air Force Research Laboratory
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.2017-0100
Reference5 articles.
1. Wick, A.T., Hooker, J.R., Walker, J., Chan, D.T., Plumley, R.W., and Zeune, C.H. "Hybrid Wing Body Performance Validation at the National Transonic Facility," AIAA-2017-####.
2. Hooker, J.R., Wick, A.T. "Design of the Hybrid Wing Body for Fuel Efficient Air Mobility Operations," AIAA-2014-1285.
3. Over Wing Nacelle Installations for Improved Energy Efficiency
4. Assessment of an unstructured-grid method for predicting 3-D turbulent viscous flows
5. Pandya, M.J., Frink, N.T., Abdol-Hamid, K.S., and Chung, J.J. "Recent Enhancements to USM3D Unstructured Flow Solver for Unsteady Flows," AIAA 2004-5201.
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