A tank is filled with water to a height H. A hole is made in one of the wall at a depth D below the water surface. The distance x from the foot of the wall at which the stream of water strikes the ground is given by :
A cylindrical tank has a hole of area 0.5 cm2 in its bottom. If the water is allowed to flow into the tank from a tube above it at the rate of 70 cm3/sec then the maximum height upto which water can rise in the tank is :
A fully loaded Boeing aircraft has a mass of \[3.3\times 10^{5} kg\]. Its total wing area is 500 m2. It is in level flight with speed of 960 kmph. Estimate the pressure difference between the lower and upper surfaces of the wings :
Figure shows a venturi meter, through which water is flowing. The speed of water at X is 2 cm/s. The speed of water at Y is :- (Take g = 1000 cm /s.s)

A large open tank has two holes in the wall. One is a square hole of side L at a depth y from the top and the other is a circular hole of radius R at a depth 4y from the top. When the tank is completely filled with water, the quantities of
water flowing out per second from the holes are both same. Then, R is equal to:
According to Torricelli's Law, the velocity of efflux from a hole at a depth hΒ is given by $$v = \sqrt{2gh}$$.
Since the volume flow rate per second
\( Q = \text{Area}\times\text{Velocity} \) is the same for both holes:
Thus, the correct option is Option 1.
A tank is filled to a height H. The range of water coming out of a hole which is a depth H/4 from the surface of water level is :
The horizontal range of water emerging from a hole is given by the formula
$$R = 2\sqrt{h(H - h)} $$