Consider the following equation, which describes the speed of sound a in an ideal gas:
a = √(kRT)
The Mach number M describes the ratio of a velocity v to the acoustic velocity or speed of sound a:
M = v/a
The Mach number can also be written in terms of the stagnation temperature T₀.
M = √[2/(k-1) ([T₀/T] - 1)]
Combine these equations and solve symbolically for the temperature T in terms of all other quantities except M. Your answer should be stored in a variable T_result, which will be a list containing one or more sympy expressions. Prefer T0 instead of T_0 in this case.