Discussion Closed This discussion was created more than 6 months ago and has been closed. To start a new discussion with a link back to this one, click here.
Undefined value found in the equation residual vector.
Posted 18 mar 2024, 20:21 GMT-4 Computational Fluid Dynamics (CFD), Studies & Solvers, Structural Mechanics 1 Reply
Please login with a confirmed email address before reporting spam
Hi all! I'm attempting to conduct a fluid-stucture simulation of an airfoil with a moving flap. I defined all my parameters and boundary conditions. I went back step-by-step and checked the boundary conditions and also the solid properties (such as Poissons ratio) and these haven't solved this error. What could I be doing wrong? Any advice is appreciated. Thanks!
Here's my setup: I have an airfoil in a air box
Laminar Flow (Air normal inflow velocity at 200m/s) Initial pressure: 101325Pa Noslip wall condition Outlet pressure total condition: 101325Pa
Solid Mechanics (wing is aluminum, used material defining properties)
Parametric sweep changing angle of flap on wing
Please login with a confirmed email address before reporting spam
I also read through this post: https://www.comsol.com/forum/thread/18191/Undefined-value-found-in-the-equation-residual-vector
To no avail, these suggestions have not helped yet.