Over Wing Nacelle Installations for Improved Energy Efficiency
Author:
Affiliation:
1. Lockheed Martin Corporation
2. Air Force Research Laboratory
3. Sandia National Laboratories
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.2013-2920
Reference21 articles.
1. Bower,R.E."OpportunitiesforAerodynamic-DragReduction."NASASP-372,1975.
2. Kinney, D.J., Hahn, A.S., and Gelhausen P.A. "Comparison of Low and High Nacelle SubsonicTransportConfigurations." AIAA97-2318.
3. Fujino, M. and Kawamura, Y. "Wave-Drag Characteristics of an Over-the-Wing Nacelle Business-JetConfiguration." JournalofAircraft, Vol40No6December2003.
4. Aerodynamic Investigations of an Advanced Over-the-Wing Nacelle Transport Aircraft Configuration
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