An aircraft of mass $3 \times 10^5 \ kg$ with total wing area $400 \ m^2$ is in a level flight at a speed of $540 \ km \ h^{-1}$. The density of air at its height is $1.2 \ kg \ m^{-3}$. The fractional increase in the speed of the air on the upper surface of its wings relative to the lower surface is . . . . . . $\left(g=10 \ ms^{-2}\right)$

  • A
    $0.727$
  • B
    $0.344$
  • C
    $0.048$
  • D
    $0.277$

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Similar Questions

According to Bernoulli's equation $\frac{P}{\rho g} + h + \frac{v^2}{2g} = \text{constant}$,the terms $\frac{P}{\rho g}$,$h$,and $\frac{v^2}{2g}$ are generally called respectively:

$A$ streamline flow of a liquid of density $\rho$ is passing through a horizontal pipe of cross-sectional area $A_1$ and $A_2$ at two ends. If the pressure of the liquid is $P$ at a point where the flow speed is $v$,then the pressure at another point where the flow speed becomes $3v$ is:

Different heads are in Column - $I$ and their formulas are given in Column - $II$. Match them appropriately.
Column - $I$Column - $II$
$(a)$ Velocity head$(i)$ $\frac{P}{\rho g}$
$(b)$ Pressure head$(ii)$ $h$
$(c)$ Potential head$(iii)$ $\frac{v^2}{2g}$

The venturi-meter works on:

What is a venturi-meter? Explain its construction and working.

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