Using Computational Fluid Dynamics and Experiments to Design Sweeping Jets for High Reynolds Number Cruise Configurations
Author:
Affiliation:
1. NASA Langley Research Center
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.2016-3311
Reference27 articles.
1. Enhancements to the FAST-MAC Circulation Control Model and Recent High-Reynolds Number Testing in the National Transonic Facility
2. Chan, D. T., Milholen II, W. E., Jones, G. S., Goodliff, S. G. "Thrust Removal Methodology for the FAST-MAC Circulation Control Model Tested in the National Transonic Facility", AIAA Paper 2014-2402.
3. High-Reynolds Number Circulation Control Testing in the National Transonic Facility (invited)
4. Development of the Circulation Control Flow Scheme used in the NTF Semi-Span FAST-MAC Model
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