dp26
Aerospace
- Nov 28, 2011
- 1
I am using shell elements for a steady state heat transfer analysis problem. I am using temperature boundary conditions and I want the total surface heat flux on a particular surface. I tried using
*SECTION PRINT and SOH, but it gave me this error,
***ERROR: THE SURFACE USED TO DEFINE SECTION REARFACE IS DEFINED USING
NON-CONTINUUM ELEMENTS. THIS IS NOT ALLOWED. PLEASE CHECK DATA.
Any help would be greatly appreciated!!
*SECTION PRINT and SOH, but it gave me this error,
***ERROR: THE SURFACE USED TO DEFINE SECTION REARFACE IS DEFINED USING
NON-CONTINUUM ELEMENTS. THIS IS NOT ALLOWED. PLEASE CHECK DATA.
Any help would be greatly appreciated!!