Explaining Continuity Equation for Jet Engines

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SUMMARY

The continuity equation is essential for understanding how jet engines generate forward thrust by conserving mass. The equation, represented as \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, describes the relationship between density and velocity in a fluid. It states that the rate of change of density within a fixed volume equals the net mass flux across its boundary. When mass flow in equals mass flow out, the density remains constant, indicating no accumulation or depletion of mass.

PREREQUISITES
  • Understanding of fluid dynamics principles
  • Familiarity with the concept of mass conservation
  • Basic knowledge of vector calculus
  • Experience with jet engine mechanics
NEXT STEPS
  • Study the application of the continuity equation in fluid dynamics
  • Explore the Navier-Stokes equations for a deeper understanding of fluid motion
  • Learn about the thermodynamics of jet engines
  • Investigate the relationship between thrust and mass flow rate in jet propulsion
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Aerospace engineers, physics students, and anyone interested in the mechanics of jet propulsion will benefit from this discussion.

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.

[tex] \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[/tex]

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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