JEE Main & Advanced Physics Fluid Mechanics, Surface Tension & Viscosity / द्रव यांत्रिकी, भूतल तनाव और चिपचिपापन Question Bank Fluid Flow

  • question_answer
    Air is streaming past a horizontal air plane wing such that its speed in 120 m/s over the upper surface and 90 m/s at the lower surface. If the density of air is 1.3 kg per metre3 and the wing is 10 m long and has an average width of 2 m, then the difference of the pressure on the two sides of the wing of

    A)            4095.0 Pascal                       

    B)            409.50 Pascal                       

    C)            40.950 Pascal                       

    D)             4.0950 Pascal

    Correct Answer: A

    Solution :

                       From the Bernoulli's theorem                    \[{{P}_{1}}-{{P}_{2}}=\frac{1}{2}\rho (v_{2}^{2}-v_{1}^{2})\]\[=\frac{1}{2}\times 1.3\times [{{(120)}^{2}}-{{(90)}^{2}}]\]            \[=4095\,N/{{m}^{2}}\]or Pascal


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