Premier Aerodynamics Podcast

How Mach Number, Angle of Attack, and Shock Waves affect boundary layer transitions - Podcast #107


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Boundary layer transitions are important. This podcast discusses how the mach number, angle of attack, and shock waves affect this transition from laminar to turbulence.
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Werq Kevin MacLeod (incompetech.com) Licensed under Creative Commons: By Attribution 3.0 License http://creativecommons.org/licenses/by/3.0/
Paper and thumbnail: https://www.mdpi.com/2227-9717/10/10/2078, Licensed under creative commons: https://creativecommons.org/licenses/by/4.0


#CFD #Aerodynamics #Turbulence #Laminar #BoundaryLayer

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Premier Aerodynamics PodcastBy Premier Aerodynamics