I have an flexible MBD model of an airctaft and a loadcase for air pressure in the form of distributed loads normal to the aircraft elements. I understand that using modal forces I can insert the load to the flexbody but only direction-wise i.e., if the load acts in all three coordinates, I 'd have to specify the load for each one.
However I only have the distributed load in the form of it beeing normal to each element. Is there a way to instert this load to Adams directly or must I find a way to break the load down to three components and insert them individually?
I suppose the load is defined by PLOAD4 cards, right? Note, it would also work with nodal forces (FORCE cards).
All you need to do is to define SUBCASE and LOAD to select the load set (SID) of your distributed load and generate MNF with residual vectors (RESVEC).
Make sure to have additional QSET and SPOINT entries required to be used with the residual vectors. You should get additional modes related to the subcases.
In *.f06 file verify that the summary says: "Modal Loads Yes"
In Adams you need to create modal force with "Define Using Function" and define scale factor to your load case defined in BDF file.
Note that in MSC Germany we developed more elaborated method which allows you to define state varying distributed load on a flap / wing surface (as a function of flap angle). In case you are interested in that solution, please contact your MSC representative.
Thank you very much, this is indeed helpful. However, I am not particularly good a Nastran user and the headers I use are pre-defined by the pre-processing program I use. While I have heard of QSETS and SPOINTS before I do not know how to set up the body to incorporate the loads the way you mention.
If possible, could you provide a model and header example of a benchmark problem? Any small flexbody mnf would do so long as there is a modal load applied.
Thanks in Advance and thank you regardless, this was very helpful,
please find attached the example. Note, I had to use PARAM,AUTOQSET,YES instead of SPOINT/QSET1 since it gives some strange number of modes. One should get 24 modes = 10 Fixed Boundary Normal modes + 13 Constrained modes + 1 residual vector mode (Modal Loadcase).
Note, there are some very useful SimCompanion articles pertinent to the topic: