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Category > Applied Sciences Posted 07 Jun 2017 My Price 5.00

Consider a flat plate at an angle of attack α to a Mach 2.4 airflow at 1 atm pressure

9.5     Consider a flat plate at an angle of attack α to a Mach 2.4 airflow at 1 atm pressure. What is the maximum pressure that can occur on the plate surface and still have an attached shock wave at the leading edge? At what value of α does this occur?

9.6     A 30.2◦ half-angle wedge is inserted into a freestream with M∞ = 3.5 and p∞ = 0.5 atm. A Pitot tube is located above the wedge surface and behind the shock wave. Calculate the magnitude of the pressure sensed by the

Pitot tube.

 

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Alpha Geek
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Status NEW Posted 07 Jun 2017 08:06 AM My Price 5.00

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