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A Kingfisher aircraft is flying in level flight, at a speed of 200 km/hr through the air (density, ρ = 1.2 kg/m3, viscosity, μ = 1.6 × 10–5 N-s/m2). The lift co-efficient at this speed is 0.4, the drag co-efficient is 0.0065 and the mass of the aircraft is 800 kg. The effective lift area (in m2) of the aircraft is ______. (Answer up to one decimal place)Correct answer is '10.6'. Can you explain this answer? for Civil Engineering (CE) 2024 is part of Civil Engineering (CE) preparation. The Question and answers have been prepared according to the Civil Engineering (CE) exam syllabus. Information about A Kingfisher aircraft is flying in level flight, at a speed of 200 km/hr through the air (density, ρ = 1.2 kg/m3, viscosity, μ = 1.6 × 10–5 N-s/m2). The lift co-efficient at this speed is 0.4, the drag co-efficient is 0.0065 and the mass of the aircraft is 800 kg. The effective lift area (in m2) of the aircraft is ______. (Answer up to one decimal place)Correct answer is '10.6'. Can you explain this answer? covers all topics & solutions for Civil Engineering (CE) 2024 Exam. Find important definitions, questions, meanings, examples, exercises and tests below for A Kingfisher aircraft is flying in level flight, at a speed of 200 km/hr through the air (density, ρ = 1.2 kg/m3, viscosity, μ = 1.6 × 10–5 N-s/m2). The lift co-efficient at this speed is 0.4, the drag co-efficient is 0.0065 and the mass of the aircraft is 800 kg. The effective lift area (in m2) of the aircraft is ______. (Answer up to one decimal place)Correct answer is '10.6'. Can you explain this answer?.

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Here you can find the meaning of A Kingfisher aircraft is flying in level flight, at a speed of 200 km/hr through the air (density, ρ = 1.2 kg/m3, viscosity, μ = 1.6 × 10–5 N-s/m2). The lift co-efficient at this speed is 0.4, the drag co-efficient is 0.0065 and the mass of the aircraft is 800 kg. The effective lift area (in m2) of the aircraft is ______. (Answer up to one decimal place)Correct answer is '10.6'. Can you explain this answer? defined & explained in the simplest way possible. Besides giving the explanation of A Kingfisher aircraft is flying in level flight, at a speed of 200 km/hr through the air (density, ρ = 1.2 kg/m3, viscosity, μ = 1.6 × 10–5 N-s/m2). The lift co-efficient at this speed is 0.4, the drag co-efficient is 0.0065 and the mass of the aircraft is 800 kg. The effective lift area (in m2) of the aircraft is ______. (Answer up to one decimal place)Correct answer is '10.6'. Can you explain this answer?, a detailed solution for A Kingfisher aircraft is flying in level flight, at a speed of 200 km/hr through the air (density, ρ = 1.2 kg/m3, viscosity, μ = 1.6 × 10–5 N-s/m2). The lift co-efficient at this speed is 0.4, the drag co-efficient is 0.0065 and the mass of the aircraft is 800 kg. The effective lift area (in m2) of the aircraft is ______. (Answer up to one decimal place)Correct answer is '10.6'. Can you explain this answer? has been provided alongside types of A Kingfisher aircraft is flying in level flight, at a speed of 200 km/hr through the air (density, ρ = 1.2 kg/m3, viscosity, μ = 1.6 × 10–5 N-s/m2). The lift co-efficient at this speed is 0.4, the drag co-efficient is 0.0065 and the mass of the aircraft is 800 kg. The effective lift area (in m2) of the aircraft is ______. (Answer up to one decimal place)Correct answer is '10.6'. Can you explain this answer? theory, EduRev gives you an ample number of questions to practice A Kingfisher aircraft is flying in level flight, at a speed of 200 km/hr through the air (density, ρ = 1.2 kg/m3, viscosity, μ = 1.6 × 10–5 N-s/m2). The lift co-efficient at this speed is 0.4, the drag co-efficient is 0.0065 and the mass of the aircraft is 800 kg. The effective lift area (in m2) of the aircraft is ______. (Answer up to one decimal place)Correct answer is '10.6'. Can you explain this answer? tests, examples and also practice Civil Engineering (CE) tests.