Recent content by drftr87

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    Can You Prove the Steady Flow Equation for Ideal Gases?

    t= temperature p= pressure n can be written as gamma(γ) which is 1.4 ive found out that t1/t2 = 1+((γ-1)/2)(m^2) where m is the mach number
  2. D

    Can You Prove the Steady Flow Equation for Ideal Gases?

    Does anybody know how to prove this equation t1/t2 = (p1/p2)^(n-1/n) thanks