Physics, 09.01.2020 05:31, recklessunreached

For the wing foil, dtermine the aerodynamic lift. density
ofair=1.21 kg/m3. area= 200m2.
speed=150m/s, speed=100m/s.

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For the wing foil, dtermine the aerodynamic lift. density
ofair=1.21 kg/m3. area= 200m2.
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