- #1
Andy_M
- 1
- 0
Hi,
I'm wondering how to calculate the center of pressure for a rocket.
More precisely, i know that the C P is located on the axis of the nozzle but i don't know how to located it on this axis...
With FLUENT and a 3d simulation, Fluent can't located it (Fluent gives me 2 differents locations on the X-axis)...
Does it exist a simple relation for find it ?
Thanks for your help,
Andy
I'm wondering how to calculate the center of pressure for a rocket.
More precisely, i know that the C P is located on the axis of the nozzle but i don't know how to located it on this axis...
With FLUENT and a 3d simulation, Fluent can't located it (Fluent gives me 2 differents locations on the X-axis)...
Does it exist a simple relation for find it ?
Thanks for your help,
Andy