Optimal artificially blunted leading-edge airfoils for enhanced aerothermodynamic performance
Author:
Affiliation:
1. Georgia Institute of Technology, Atlanta, Georgia 30332-0150
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Space and Planetary Science,Aerospace Engineering
Link
https://arc.aiaa.org/doi/pdf/10.2514/3.27191
Reference18 articles.
1. AERODYNAMIC DESIGN FOR SUPERSONIC SPEEDS
2. Supersonic channel-airfoils for reduced drag
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