This survey was prepared for having a structured compendium about the aerodynamic characteristics of several supercritical airfoils. It may be used within the scope of the design of commercial airliners. The survey is based on published data coming from wind tunnel tests performed at the NASA Langley 0.3-Meter Transonic Cryogenic Tunnel. All of the referenced reports are published on the NASA Technical Reports Server (NTRS).
Bundesministerium für Forschung, Technologie und Raumfahrt