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Cfd Analysis of Convergent- Divergent Supersonic Nozzle<br />

Fig. 4.6: Velocity Contours With 4mm Axial Gap Between Nozzle and rotor blades.<br />

Fig. 4.7: Velocity contours with 5mm axial gap between nozzle and rotor blades.<br />

Fig 4.8 Velocity vectors with 3mm Axial gap between Nozzle and Rotor blades.<br />

Fig. 4.9: Velocity vectors with 4mm Axial gap between Nozzle and Rotor blades.<br />

Fig. 4.10: Velocity vectors with 5mm Axial gap between Nozzle and Rotor blades.<br />

Fig. 4.11: Tangential velocity contours with 3mm axial gap between Nozzle and Rotor blades.<br />

www.<strong>ijcer</strong>online.com ||May ||2013|| Page 14

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