\"\"

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a.

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Find the angle \"\".

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The equation is \"\".

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Half-angle identity : \"\".

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\"\".

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Since the mach number describing a plane\"\"s speed cannot be negative, \"\".

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\"\"

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b.

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Consider \"\".

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Substitute the values of \"\" in \"\".

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\"\"

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The mach number of the plane is about 3.2.

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\"\"

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a. \"\".

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b. The mach number of the plane is about 3.2.