(b) An aircraft weighing 1337 kN when fully loaded has a wing area of 226 m2. It is to take off at velocity of 300 km/h. Assume the airport is at 3000m above sea level. The wing has the characteristics of an airfoil shown below (C vs a). What is (a) the necessary angle of attack and induced drag coefficient if the wing span is 30m. The pressure variation in the atmosphere is given as: p = Ps (1 6.5K Ts = km dT Where R is the gas constant for air, a is the lapse rate dz (15+273)K, R=287 J/K/kg, subscript s=sea-level. Ps=101.325KP.. Chord 0.48 0.40 0.32 1.6 0.24 1.2 0.8 0.16 Ce 0.08 0.4 0.4 16 24 32 Angle of attack, a (degrees) Lift coefficient, CL Drag coefficient, C,

(b) An aircraft weighing 1337 kN when fully loaded has a wing area of 226 m2. It is to take off at velocity of 300 km/h. Assume the airport is at 3000m above sea level. The wing has the characteristics of an airfoil shown below (C vs a). What is (a) the necessary angle of attack and induced drag coefficient if the wing span is 30m. The pressure variation in the atmosphere is given as: p = Ps (1 6.5K Ts = km dT Where R is the gas constant for air, a is the lapse rate dz (15+273)K, R=287 J/K/kg, subscript s=sea-level. Ps=101.325KP.. Chord 0.48 0.40 0.32 1.6 0.24 1.2 0.8 0.16 Ce 0.08 0.4 0.4 16 24 32 Angle of attack, a (degrees) Lift coefficient, CL Drag coefficient, C,

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Description: (b) An aircraft weighing 1337 kN when fully loaded has a wing area of 226 m2. It is totake off at velocity of 300 km/h. Assume the airport is at 3000m above sea level.The wing has the characteristics of an airfoil shown below (CL vs a). What is (a)t

College Physics

11th Edition

ISBN:9781305952300

Author:Raymond A. Serway, Chris Vuille

Publisher:Raymond A. Serway, Chris Vuille

Chapter1: Units, Trigonometry. And Vectors

Section: Chapter Questions

Problem 1CQ: Estimate the order of magnitude of the length, in meters, of each of the following; (a) a mouse, (b)...

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