Question: 5 . ( 2 0 points ) Assuming no losses, calculate the Mach number, dynamic pressure, and dynamic temperature at the tail of the aircraft.

5 . (20

points

)

Assuming no losses, calculate the Mach number, dynamic pressure, and dynamic temperature at the tail of the aircraft. Note that the illustration is not to scale.

\ ((

= 1.4 \)

and

\ (

= 287 \)

/

.

)

5 . ( 2 0 points ) Assuming no losses, calculate

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