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What is the value that maintains minimum power speed of the aircraft?(a) u/\(\sqrt[4]{3}\)(b) u/\(\sqrt[3]{3}\)(c) u^2/\(\sqrt[4]{3}\)(d) u^2/\(\sqrt[3]{3}\)The question was asked in unit test.My question is based upon Climb and Descent Performance with Thrust-Producing Engines topic in chapter Climb and Descent Performance of Aircraft Performance |
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Answer» The CORRECT option is (a) u/\(\sqrt[4]{3}\) |
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