should gain a knowledge of how they simulate supersonic flow in a convergent – Divergent Nozzle, shown in Figure 1(a), using ANSYS–Fluent. Then compare the obtained computational results with hand calculation results using table for isentropic flow [page 417] and Table for Normal shock wave [page 429]. In the simulation part which will be submitted in project Page5of16 deliverable 2, student will simulate a uniform supersonic stream flow in C-D nozzle as shown in the Figure1 (b)