Transonic Semispan Aerodynamic Testing of the Hybrid Wing Body with Over Wing Nacelles in the National Transonic Facility
Author:
Affiliation:
1. NASA Langley Research Center
2. Lockheed Martin Corporation
3. Air Force Research Laboratory
4. Jacobs Technology, Inc.
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.2017-0098
Reference34 articles.
1. Over Wing Nacelle Installations for Improved Energy Efficiency
2. Next Generation Civil Transport Aircraft Design Considerations for Improving Vehicle and System-Level Efficiency
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