Force acting on a flat plate that is moving trough fluid

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SUMMARY

The discussion focuses on calculating the force acting on a flat plate moving through air, specifically for rocket simulation involving flat stabilizers. The user initially proposed a formula, F = q*v*P, where q represents fluid density, v is velocity, and P is the plate area in square meters. However, the correct formula provided is F = 0.5 * Cd * q * v^2 * P, where Cd is the drag coefficient, which accounts for the aerodynamic effects on the plate.

PREREQUISITES
  • Understanding of fluid dynamics principles
  • Familiarity with drag coefficients (Cd)
  • Knowledge of basic physics formulas related to force
  • Experience with rocket simulation concepts
NEXT STEPS
  • Research the calculation of drag coefficients for various shapes
  • Explore fluid dynamics simulations using software like ANSYS Fluent
  • Learn about the effects of plate orientation on aerodynamic forces
  • Investigate the impact of varying fluid densities on force calculations
USEFUL FOR

Aerospace engineers, physics students, and anyone involved in rocket design or fluid dynamics simulations will benefit from this discussion.

deluksic
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soo as the title says, i need formula for force acting on a plate that is moving trough fluid, in my case air... need it for rocket simulation because of its flat stabilizers...

i thought like this:

a flat plate is moving in any direction (yeah that complicates things... but keep it simple) so i get the normal component of speed on the plate, then i calc somthing like this:

F = q*v*P where q is density of fluid, v is velocity, and P is size of plate (m2)

**plate has no width... in my case**

thats kinduh dum formula but i need real one :D
 
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Try

F = 0.5 X Cd X q X v^2 X P

where variables are as you selected above and Cd is the drag coefficient.
 

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