Recent content by luk3tm

  1. L

    TThermodynamics-compressed flow in a nozzle equation derivation

    okay so i think I've almost got it but i might be missing out on something: Vstar/V=Ap/Astar*pstar substituting in mac number, Mcstar/Mcr=RHS substituting C=sqrt(KRT) gives: M/Msqrt(KRTstar/KRT) =sqrt(T*/T) Tstar/T=Tstar/To*To/T=(1+k-1/2)M*2*2/k+1 and...
  2. L

    TThermodynamics-compressed flow in a nozzle equation derivation

    Hi everyone! Homework Statement Just one part of the lecture notes I couldn't work out how to derrive (apparently we need to know how). A/A*=1/M[2/(k+1)(1+(k-1)/2*M^2)]^(k+1/2(k-1))Homework Equations A/A*=1/M[2/(k+1)(1+(k-1)/2*M^2)]^(k+1/2(k-1)) ρ0/ρ=[1+(k-1/2)*M^2]^(1/k-1)...
Back
Top