Explaining Continuity Equation for Jet Engines

AI Thread Summary
The continuity equation describes the conservation of mass in a jet engine, indicating that the rate of change of density within a fixed volume is equal to the net mass flux across its boundaries. In simpler terms, if the mass flow into the engine equals the mass flow out, the density remains constant, meaning there’s no accumulation or loss of mass. This principle is crucial for understanding how jet engines generate forward thrust by expelling exhaust gases. The balance of mass flow is essential for maintaining efficient engine operation. Understanding this concept is key to grasping the mechanics of jet propulsion.
Penn_State21
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I have this one as well, using the continuity equation to explain how a jet engine provides a foward thrust for an airplane. I have the equation but can some one explain this to me in laymen's terms.

<br /> \frac{\partial\rho\left(\vec{r},t\right)}{\partial t}+\nabla\cdot\left[\rho\left(\vec{r},t\right)\vec{v}\left(\vec{r},t\right)\right]= 0

Thanks in advance for your help.

Kris
 
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The continuity equation is an equation related to conservation of mass.

The rate of change of density (in a constant volume) is equal the net mass flux across the boundary of a differential volume.

If the net flux is zero, i.e. the mass flow in = mass flow out, then there is no change in density (and no accumulation or decrease in mass) in a fixed volume.
 
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