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Air enters a 5 cm diameter frictionless duct with a Mach number 2. Its static temperature is 250 0C and stagnation pressure 6 bar. For increasing Mach number to 3, find the amount of heat to be transferred and change in static temperature. You may use the following table for air having g=1.4:

     

M

T/T*

P/P*

Po/Po*

To/To*

2

0.5289

0.3636

1.503

0.7934

3

0.2803

0.1765

3.424

0.6534

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