Explained: Oblique Shock Relations Derivation
In this video, we will derive the oblique shock (OS) relations. We will start from integral conservation equations, and derive expressions for the downstream Mach number, density ratio, velocity ratio, pressure ratio, and temperature ratio. ===== RELEVANT VIDEOS ===== → Oblique Shock Example https://goo.gl/77hjcb → Normal Shock Relations Derivation https://goo.gl/Unvjey → Normal Shock Example https://goo.gl/RBJtgV ===== RELEVANT LINKS ===== ► Surface (Double) Integrals Explanation http://www.joshtheengineer.com/2017/0... ► VT Calculator http://www.dept.aoe.vt.edu/~devenpor/... ► MATLAB Functions https://github.com/jte0419/Compressib... ===== THUMBNAIL CREDIT ===== By Settles1 (Own work) [CC BY-SA 4.0 (https://creativecommons.org/licenses/...)], via Wikimedia Commons

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Oblique shocks and expansion fans [Aerodynamics #19]

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