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Discussion :: GATE Aeronautical Engineering

  1. Consider a supersonic stream at a Mach number M=2, undergoing a gradual expansion. The stream is turned by an angle of 3 degrees due to the expansion. The following data is given.
      
    The Mach number downstream of the expansion is
    2. A.
    1.88
    B.
    2.00
    C.
    2.11
    D.
    2.33

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    Workspace

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    Answer : Option C

    Explanation :

    -NA-

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