MIT OpenCourseWare | Aeronautics and Astronautics | 16.100 (Www.OSIR.org.in)
16.100 generally has four components: subsonic potential flows, including source/vortex panel methods; viscous flows, including laminar and turbulent boundary layers; aerodynamics
Source: ocw.mit.edu
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Source: www.yourwayautobody.com
