Thick supercritical airfoils with low drag and natural laminar flow
Author:
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/3.45460
Reference14 articles.
1. BOUNDARY LAYER TRANSITION- FREESTREAM TURBULENCE AND PRESSURE GRADIENT EFFECTS
2. Supercritical Wing Sections III
3. Development of modern airfoil sections for high subsonic cruise speeds
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