Effects of the Shock Wave Structure on the Tip Clearance Leakage Flow in Transonic Compressor Rotors

<div>Distribution of the flow parameters at the tip clearance of RotorSD. (a) Distributions of the pressure difference. (b) Distributions of relative velocity perpendicular to the pressure surface at the blade tip.</div>

International Journal of Aerospace Engineering

fig27

Figure 27

Figure 27: Effects of the Shock Wave Structure on the Tip Clearance Leakage Flow in Transonic Compressor Rotors 