Expanding the Natural Laminar Flow Boundary for Supersonic Transports
Author:
Affiliation:
1. NASA Langley Research Center
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.2016-4327
Reference15 articles.
1. On the Flow Along Swept Leading Edges
2. Some observations of the transition process on the windward face of a long yawed cylinder
3. Supersonic Testing of Natural Laminar Flow on Sharp Leading Edge Airfoils. Recent Experiments by Aerion Corporation
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