Hi David,
So here are my more detailed observations related to your models.
You have attached 2 files - both using Newmark acceleration method, one with acceleration excitation using "Direction X", another with analogous nodal accelerations. They were expected to give similar results but they didn't.
First as concerns the model with "Direction X" excitation:
1/ In Message 2 of this forum topic I have written "the factor should be equal to gravity acceleration expressed in m/s2 so 9.80665 m/s2". It is independent from units used in the project - I know it is unexpected, especially for someone using imperial units 😞 So it was necessary to change the factor from 32.2 (corresponding to ft/s2) to 9.80665 (corresponding to m/s2)
Then as concerns the model with nodal acceleration excitation:
2/ Load case 1, used in this excitation, contained not only imposed nodal acceleration but also the self-weight load. In such case the self-weight load was also multiplied by the forcing function "4Z_acc". It was necessary to delete the self-weight load from load case 1 to avoid this effect.
3/ The imposed nodal acceleration load in load case 1 was applied to nodes where added masses were defined. Any imposed acceleration, velocity or displacement loads should be applied to supported nodes (and moreover to fixed directions in these supports) - in opposite case they do not work. It was necessary to replace the loaded nodes by nodes where supports were defined by you.
Now as concerns more general remarks related to both models:
4/ You have defined damping as 0.05 for Alpha. In case of Newmark acceleration, Newmark or HHT methods damping matrix is defined as the linear combination of mass matrix and stiffness matrix with Alpha and Beta coefficients respectively. So Alpha=0.05 does not correspond to 0.05 relative damping (5%) which you probably indended. Alpha and Beta corresponding to such damping can be calculated using the "calculator" available in the bottom part of Rayleigh Damping window - necessary to specify relative damping values for some represenattive pulsations omega (frequencies expressed in radian/s instead of Hz - multiplied by 2*PI). To avoid doubts I have specified no damping.
5/ As I have noticed before your forcing function contained not only the acceleration impulse but also some constant acceleration before the impulse (from t=0 seconds) and after it. It corresponds to applying some constant load to the unsupported structure resulting in rigid body movement with constant acceleration - so not resulting in any internal forces (except of transient effects when applying such load at t=0s). That is why I modified the forcing function leaving only the acceleration impulse and "moving" it close to t=0s.
6/ The acceleration impulse in the forcing function is also very "artificial" because it contains only positive acceleration. In your last answer you have mentioned RMS values of accelerations - time history analysis expects excitation defined in the time (not frequency) domain without any statistical processing - it should be physical values.
According to above points I have modified your model. I have also defined the 3rd one - using "Direction X" excitement and Modal Decomposition method (this one also without damping).
Then I have run analysis of them and checked some results - reaction in one of supported nodes and von Mises stress in the center of one of finite elements.
Results in all 3 models are very close - see the screen captures below.



I have also attached the models - without results to reduce the size.
When checking displacements in the model with imposed nodal acceleration you can see that it is a superposition of displacements resulting from deformations caused by vibrations and displacements (much bigger than the first ones) caused by rigid body movement of all structure. The acceleration impulse contains only posititive accelerations so after ending it the non-zero velocity of structure remains. As I have mentioned before the "Base-line correction" is not implemented in Robot so it is not possible to separate in it this rigid body movement and deformations.
I hope these too long explanations will be useful:)
Regards,
Pawel Pulak
Technical Account Specialist