Page 136 - 48Fundamentals of Compressible Fluid Mechanics
P. 136
98 CHAPTER 5. NORMAL SHOCK
5.5 Shock with Real Gases
5.6 Shock in Wet Steam
5.7 Normal Shock in Ducts
The flow in ducts is related to boundary layer issues. For a high Reynolds number,
the assumption of uniform flow in the duct is closer to reality. It is normal to have
a large Mach number with a large Re number. In that case, the assumptions in
construction of these models are acceptable and reasonable.
5.8 Tables of Normal shocks, Ideal Gas
Table 5.1: The shock wave Table for k = 1.4
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