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An aircraft is flying in level flight at a speed of 200 km/hr through air (Density, ρ = 1.2 kg/m3 and viscosity, m = 1.6 × 10-5 N-s/m2). The lift co-efficient at this speed is 0.4 and the drag co-efficient is 0.0065. 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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    An aircraft is flying in level flight at a speed of 200 km/hr through...
    Aircraft generates the lift equal to the weight of the aircraft, so at the equilibrium condition.
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    An aircraft is flying in level flight at a speed of 200 km/hr through air (Density, ρ = 1.2 kg/m3 and viscosity, m = 1.6 × 10-5 N-s/m2). The lift co-efficient at this speed is 0.4 and the drag co-efficient is 0.0065. 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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    An aircraft is flying in level flight at a speed of 200 km/hr through air (Density, ρ = 1.2 kg/m3 and viscosity, m = 1.6 × 10-5 N-s/m2). The lift co-efficient at this speed is 0.4 and the drag co-efficient is 0.0065. 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 Electrical Engineering (EE) 2024 is part of Electrical Engineering (EE) preparation. The Question and answers have been prepared according to the Electrical Engineering (EE) exam syllabus. Information about An aircraft is flying in level flight at a speed of 200 km/hr through air (Density, ρ = 1.2 kg/m3 and viscosity, m = 1.6 × 10-5 N-s/m2). The lift co-efficient at this speed is 0.4 and the drag co-efficient is 0.0065. 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 Electrical Engineering (EE) 2024 Exam. Find important definitions, questions, meanings, examples, exercises and tests below for An aircraft is flying in level flight at a speed of 200 km/hr through air (Density, ρ = 1.2 kg/m3 and viscosity, m = 1.6 × 10-5 N-s/m2). The lift co-efficient at this speed is 0.4 and the drag co-efficient is 0.0065. 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?.
    Solutions for An aircraft is flying in level flight at a speed of 200 km/hr through air (Density, ρ = 1.2 kg/m3 and viscosity, m = 1.6 × 10-5 N-s/m2). The lift co-efficient at this speed is 0.4 and the drag co-efficient is 0.0065. 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? in English & in Hindi are available as part of our courses for Electrical Engineering (EE). Download more important topics, notes, lectures and mock test series for Electrical Engineering (EE) Exam by signing up for free.
    Here you can find the meaning of An aircraft is flying in level flight at a speed of 200 km/hr through air (Density, ρ = 1.2 kg/m3 and viscosity, m = 1.6 × 10-5 N-s/m2). The lift co-efficient at this speed is 0.4 and the drag co-efficient is 0.0065. 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 An aircraft is flying in level flight at a speed of 200 km/hr through air (Density, ρ = 1.2 kg/m3 and viscosity, m = 1.6 × 10-5 N-s/m2). The lift co-efficient at this speed is 0.4 and the drag co-efficient is 0.0065. 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 An aircraft is flying in level flight at a speed of 200 km/hr through air (Density, ρ = 1.2 kg/m3 and viscosity, m = 1.6 × 10-5 N-s/m2). The lift co-efficient at this speed is 0.4 and the drag co-efficient is 0.0065. 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 An aircraft is flying in level flight at a speed of 200 km/hr through air (Density, ρ = 1.2 kg/m3 and viscosity, m = 1.6 × 10-5 N-s/m2). The lift co-efficient at this speed is 0.4 and the drag co-efficient is 0.0065. 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 An aircraft is flying in level flight at a speed of 200 km/hr through air (Density, ρ = 1.2 kg/m3 and viscosity, m = 1.6 × 10-5 N-s/m2). The lift co-efficient at this speed is 0.4 and the drag co-efficient is 0.0065. 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 Electrical Engineering (EE) tests.
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