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

Premier Aerodynamics: https://www.youtube.com/premieraerodynamics?sub_confirmation=1 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. Want to get better at CFD? Check out our courses: https://premieraerodynamics.com/Courses/ Want an easy way to make your experiments 2-4% more accurate? Check out The Atmosphere Hawk to make your aerodynamic experiments better: https://premieraerodynamics.com/Atmosphere-hawk 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