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What is the relationship between temperature and mach number?(a) T0=T\(\Big[1+\frac{\gamma-1}{2}M^2\Big]\)(b) T0=T\(\Big[1+\frac{\gamma+1}{2}M^2\Big]\)(c) T0=T\(\Big[1-\frac{\gamma-1}{2}M^2\Big]\)(d) T0=T\(\Big[1-\frac{\gamma+1}{2}M^2\Big]\)This question was posed to me by my school teacher while I was bunking the class.I want to ask this question from Measurement of Mach Number in chapter Atmosphere and Air Data Measurement of Aircraft Performance

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Correct option is (a) T0=T\(\Big[1+\frac{\gamma-1}{2}M^2\Big]\)

The best explanation: The relationship between temperature and MACH number is T0=T\(\Big[1+\frac{\gamma-1}{2}M^2\Big]\) where T is the temperature at that ALTITUDE, T_0 is the STAGNATION temperature, M is mach number and γ is the ratio of specific heat at CONSTANT pressure to that of specific heat at constant VOLUME.



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