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2 years ago

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Consider a Mach 4.5 airflow at a pressure of 1.25 atm. We want to slow this flow to a subsonic speed through a system of shock w

aves with as small a loss in total pressure a possible. Compare the loss in total pressure for the following shock systems: a. A single normal shock wave. b. An oblique shock with a deflection angle of 23.5°, followed by a normal shock. c. An oblique shock with a deflection angle of 23.5°, followed by a second oblique shock of deflection angle 15°, followed by a normal shoc

1 answer:

marissa [1.9K]2 years ago

6 0

Answer:

a. 130.73 atm

b. 102.62 atm

c. 87.1 atm

Explanation:

See the attached pictures.

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An electric motor is to be supported by four identical mounts. Each mount can be treated as a linear prevent problems due requir

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GIVEN:

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$\frac{A}{F}$ will give the tranfer function

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3 years ago

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Answer:

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