The lift force acting on the wing of an aeroplane is $$2275$$ N . If the area of the wing is $$5$$ $$m2$$ and velocity of air on the lower surface of the wing is $$30$$ $$m/s$$ , velocity of air on the upper surface of the wing is (density$$ of air is $$1.3$$ k $$gm3$$ $$)

Question

The lift force acting on the wing of an aeroplane is $$2275$$ N     . If the area of the wing is $$5$$ $$m2$$     and velocity of air on the lower surface of the wing is $$30$$ $$m/s$$     , velocity of air on the upper surface of the wing is  (density$$ of air is $$1.3$$ k $$gm3$$     $$)

Infinity Learn · Accepted Answer

$$F=$$ρ$$A2(v22$$−$$v12)$$                          $$2275=1.3$$×$$52$$[$$v22$$−$$(30)2$$] $$v22$$−$$900=22753.25=700$$                     $$v22=1600$$⇒$$v2=40ms$$−$$1$$

The lift force acting on the wing of an aeroplane is $2275 N$ . If the area of the wing is $5 m^{2}$ and velocity of air on the lower surface of the wing is $30 m / s$ , velocity of air on the upper surface of the wing is (density of air is $1.3 k g m^{3}$ )

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The lift force acting on the wing of an aeroplane is 2275 N . If the area of the wing is 5 m2 and velocity of air on the lower surface of the wing is 30 m/s , velocity of air on the upper surface of the wing is (density of air is 1.3 k gm3 )

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The lift force acting on the wing of an aeroplane is $2275 N$ . If the area of the wing is $5 m^{2}$ and velocity of air on the lower surface of the wing is $30 m / s$ , velocity of air on the upper surface of the wing is (density of air is $1.3 k g m^{3}$ )