Aircraft data for Problems 11–15:
Landing speed = 100 knots (169 fps)
Gross weight = 8000 lb Average retarding force = 2000 lb
Sea level standard conditions
11. Calculate the deceleration.
12. Calculate the no-wind stopping distance.
13. If the weight is increased to 13,000 lb, calculate the no-wind stopping distance. Assume the same landing speed (100 knots).
14. If the 8000-lb airplane lands with a 10-knot tailwind, calculate the stopping distance.
15. If the aircraft is operating from an airfield where the density ratio is 0.8, calculate the no-wind stopping distance. Thanks!
to many question so I am solving 11,12 and 13
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