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9 10Inuing muid properties ratio at thegiven Mach number.10. If air at 1 bar and 310 K, moving at Ma=3, encounter a flow deflection of 10°, calculate thepercentage change in Mach number and pressure and wave angle. If subsequent second flowdeflection also brings about the same percentage change in pressure, find that flow deflection angle.Use shock angle (B=86.41°) and use gas table (isentropic flow and Normal shock table) for findingfluid properties ratio at the given Mach number.​

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