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Feasibility Investigation on Reduced-Power Take-Off of MA600
Abstract:
This paper investigates the feasibility of MA600 reduced-power take-off by finding the necessary conditions which reduced-power take-off must satisfy based on the performance characteristics and actual flight data of MA600 turboprop aircraft. Finally, we come to the conclusion that reduced-power take-off of MA600 aircraft can be achieved.
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486-490
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Online since:
September 2013
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© 2013 Trans Tech Publications Ltd. All Rights Reserved
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