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An aircraft with mass of 400,000 kg cruises at 240 m/s at an altitude of 10 km. Its lift to drag ratio at cruise is 15. Assuming g as 9.81 m/s2, the power (in MW) needed for it to cruise is _______ (accurate to two decimal places).Correct answer is '62.00 to 63.50'. Can you explain this answer? for GATE 2024 is part of GATE preparation. The Question and answers have been prepared
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An aircraft with mass of 400,000 kg cruises at 240 m/s at an altitude of 10 km. Its lift to drag ratio at cruise is 15. Assuming g as 9.81 m/s2, the power (in MW) needed for it to cruise is _______ (accurate to two decimal places).Correct answer is '62.00 to 63.50'. Can you explain this answer?, a detailed solution for An aircraft with mass of 400,000 kg cruises at 240 m/s at an altitude of 10 km. Its lift to drag ratio at cruise is 15. Assuming g as 9.81 m/s2, the power (in MW) needed for it to cruise is _______ (accurate to two decimal places).Correct answer is '62.00 to 63.50'. Can you explain this answer? has been provided alongside types of An aircraft with mass of 400,000 kg cruises at 240 m/s at an altitude of 10 km. Its lift to drag ratio at cruise is 15. Assuming g as 9.81 m/s2, the power (in MW) needed for it to cruise is _______ (accurate to two decimal places).Correct answer is '62.00 to 63.50'. Can you explain this answer? theory, EduRev gives you an
ample number of questions to practice An aircraft with mass of 400,000 kg cruises at 240 m/s at an altitude of 10 km. Its lift to drag ratio at cruise is 15. Assuming g as 9.81 m/s2, the power (in MW) needed for it to cruise is _______ (accurate to two decimal places).Correct answer is '62.00 to 63.50'. Can you explain this answer? tests, examples and also practice GATE tests.