Q6: An aircraft is moving at a constant speed V = 500 m/s. It is performing a vertical loop of radius R-5 km. At this in
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Q6: An aircraft is moving at a constant speed V = 500 m/s. It is performing a vertical loop of radius R-5 km. At this in
Q6: An aircraft is moving at a constant speed V = 500 m/s. It is performing a vertical loop of radius R-5 km. At this instant it is rolling at a constant rate w, = 1 rad/s. The pilot is also swinging his wings back at a constant rate w₁ = 0.5 rad/s. The centre of mass of the right wing is C and the principal radii of gyration of the right wing about C are kx = 1m, ky = 5m, k₂ = 10m. The mass of the right wing is 500 kg. What is the net moment about C applied by the plane body and the aerodynamic forces on the wing, at this instant, to enable this motion of the wing? T us="^-0·8² wwe 0 w₂= the twil, + w w 110² > of Z 12 R=5 km v V← A w₁ =1rads/s की wy-up W₁ the+ + OX w=0.5 rad/s var شدات → Y ym