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Understanding Fluid Dynamics Equations
Feb 8, 2025
Lecture Notes: Fluid and Gas Flow Equations
Key Equations Discussed
Continuity Equation
Euler Equation
Continuity Equation
Overview
Focuses on the conservation of mass in fluid flow.
Relevant for flow through channels.
Involves a streamtube formed by streamlines.
Equation Details
Assumptions:
Steady flow, ρ (density) and V (velocity) are mean values over the area.
Variables:
Station 1: Velocity ( v_1 ), Area ( A_1 )
Station 2: Velocity ( v_2 ), Area ( A_2 )
Formula:
Mass flow per second: ( \rho A V )
Continuity equation: ( \rho_1 A_1 V_1 = \rho_2 A_2 V_2 )
For incompressible flow: ( A V = \text{constant} )
Key Point
The equation states that the mass per second entering a streamtube is equal to the mass per second exiting.
Euler Equation
Overview
Based on conservation of momentum.
Applies Newton’s second law to a flowing gas.
Derivation
Consider a volume of air following a streamline with dimensions ( dx, dy, dz ).
Forces involved: pressure force, friction force, gravity force (gravity and friction neglected for the derivation).
Calculation
Pressure Force:
At left side: Pressure ( P )
At opposite side: ( P + \Delta P )
( \Delta P = \frac{dP}{dx} dx )
Resulting force in x-direction: (-\frac{dP}{dx} dx \cdot dy \cdot dz)
Mass and Acceleration:
Mass ( m = \rho \cdot dx \cdot dy \cdot dz )
Acceleration: ( a = \frac{dV}{dx} \cdot V )
Final Equation
Combining terms: ( dP = -\rho V dV )
Application:
Applies to compressible flow due to the presence of ρ.
Historical Context
Derived by Leonhard Euler, a Swiss mathematician.
Notes for Next Lecture
Discussion on Bernoulli family and further exploration on Euler's contributions.
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