AP EAMCET Engineering 17 Sep 2020 Shift 2 Paper

Section: Physics

Question : 94 of 160

Marks: +1, -0

A fully loaded Boeing air craft has a mass of 3.3×105 kg. Its total wing area is 500 m2. Itis in level flight with a speed of 960 kmph . Estimate the pressure difference between thelower and upper surfaces of the wings.

4.5×103 N.m−2
5.5×103 N.m−2
6.5×103 N.m−2
7.5×103 N.m−2

Validate

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