Bernoulli's equation for compressible fluids · RMPH 2016 #A

Physics · fluid-mechanics

Problem

The study of gases flow uncovers many interesting phenomena which have a myriad of applications, starting from boilers to airplanes and rockets. To simplify the calculations, in this problem the following assumptions will be adopted: - The gas is ideal; - The gas flow is steady and non-turbulent; - The processes taking place in the flowing gas are adiabatic; - The gas flow speed is much less than the speed of light; - The gas flow is uniform and one-dimensional (axisymmetric); - The effect of gravity is negligible. Bernoulli's equation is the mathematical form of the law of conservation and transformation of energy for a flowing ideal gas. It bears the name of the Swiss physicist Daniel Bernoulli (1700 - 1782), who derived it in 1738. The easiest way to obtain this equation is to follow a fluid particle (a volume element of the fluid) in its way on a streamline. Perform the energy balance between two points in the flowing gas, knowing the parameters pp, ρ\rho, and vv, and derive the equation that connects these variables. The adiabatic exponent γ\gamma of the gas is also known. The parameter pp is the gas pressure, ρ\rho its density, and vv its speed.

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