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  1. mano112aprmw

    Importing load from Excel

    Hi everyone am working in Hypermesh(Aerospace) profile, i want to import load from excel which has nodal coordinates(or Element ID) and XYZ component forces . How to do this?? Thanks.
  2. mano112aprmw

    ERROR # 789

    @Prakash Pagadala Hi Prakash , Sorry for the late reply , here is my OUT file opti.out
  3. mano112aprmw

    ERROR # 789

    ' *** ERROR # 789 *** Invalid design properties w.r.t. the design variables were found. number of invalid property items = 5' can u tell me what problem am facing???. There is no zero values in lower bound and upper bound
  4. mano112aprmw

    Size Optimization of Stiffened Plate.

    HI @Prakash Pagadala Here is my file ...Am using Hat section 2.hm
  5. mano112aprmw

    Size Optimization of Stiffened Plate.

    Hi @Prakash Pagadala I modeled my stiffened plate like shell element with offset beam element. Am keeping my plate thickness as constant, i want to change my thickness of stiffener(beam element) but in generic relationship there is no thickness variable. which one i should choose?
  6. mano112aprmw

    Size Optimization of Stiffened Plate.

    Is there any tutorials available for Optimization of stiffened plate. In my case my design variable is size of the stiffener and keeping dimension of the plate as constant. And constraint is, max displacement of the plate should not go 1mm..
  7. mano112aprmw

    Contact in MSc Nastran profile

    How to define a contact between two surface of shell elements in Nastran profile? Which card image i should use? I created slave and master elements using contact surface collector . Am doing linear static and normal mode analysis.
  8. mano112aprmw

    'Z' cross section in Hyperbeam

    No, am working in Ansys interface , I can't rotate the Z cross section in ansys interface but we can do in Hyperbeam
  9. mano112aprmw

    'Z' cross section in Hyperbeam

    How to get 'Z' cross section in Hyperbeam?