Question: According to the aerodynamics textbook, how does % thrust available for jet aircraft vary with % RPM? @ % thrust changes in direct proportion to

According to the aerodynamics textbook, how does % thrust available for jet aircraft vary with % RPM? @ % thrust changes in direct proportion to changes in % RPM. (O % thrust increases exponentially with increases with % RPM. O % thrust decreases with increases with % RPM. (O % thrust is unaffected by Mach number

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