ermine the Anozzle exit/A* required to achieve a Mach 5 flow at the inlet of thechannel with a cross-sectional area of 45 mm x 45 mm.2. What is the stagnation pressure needed for C-D nozzle to maintain a normal shockat the exit plane of the channel.3. How many tanks are required to run the facility for 2 mins?4. Determine the heat release for a stoichiometric combustion of hydrogen (ignoringfriction).5. Compare the stagnation pressure required for the ideally expanded scenario to thatof maintain a normal shock at the exit plane of the channel from 2 (non-reacting).225 mm45 mmC-D Nozzlef = 0.02Format: I encourage you to discuss this project with your classmates, but all formulas, analysis, computer coding, or reports should be done individually. The best way to really learn is through doing it yourself. Please show all your relevant work and steps of how you solved the problem. Regulators to hold