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Flugmechanik
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Wind-Tunnel Results for an Improved 21-Percent-Thick Low-Speed Airfoil Section
Low-Speed Wind Tunnel Results for a Modified 13-Percent-Thick Airfoil
Transonic Aerodynamic Characteristics of the 10-Percent-Thick NASA Supercritical Airfoil 31
Aerodynamic Characteristics of an Improved 10-Percent-Thick NASA Supercritical Airfoil