Punjab Medical Punjab - MET Solved Paper-2008

  • question_answer
    The pressure on the top surface of an aeroplane wing is \[0.8\times {{10}^{5}}\] Pa and the pressure on the bottom surface is \[0.75\times {{10}^{5}}\] Pa. If the area of each surface is\[50\,\,{{m}^{2}}\], the dynamic lift on the wing is

    A) \[25\times {{10}^{4}}N\]                              

    B) \[0.5\times {{10}^{4}}N\]

    C) \[5\times {{10}^{4}}N\]                

    D) \[0.25\times {{10}^{5}}N\]

    Correct Answer: A

    Solution :

    Dynamic lift on the wing                 \[F=({{P}_{1}}-{{P}_{2}})A\]                     \[=(0.8\times {{10}^{5}}-0.75\times {{10}^{5}})\times 50\]                     \[=0.05\times {{10}^{5}}\times 50=25\times {{10}^{4}}N\]


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