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What is the value of ‘n’ exponential in the fuel flow law for a high bypass ratio turbofan?(a) 0.4(b) 0.5(c) 0.6(d) 0.7I got this question by my college professor while I was bunking the class.I'd like to ask this question from Cruising Performance in chapter Cruising Performance of Aircraft Performance |
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Answer» The correct answer is (c) 0.6 |
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