2 thoughts on “Mod-01 Lec-16 Design of Compressor Blades, Aerofoil Design (Subsonic, Transonic, Supersonic)

  1. How do we calculate C_w1m @15:00 and also C_w2m later in the slides? I can understand how U, W_th, and C_a are known apriori. Am I missing something here?

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