Aeroelasticity vs. Hand Calculations: Read our in-depth case study that covers generating aerodynamic loads for a Fokker Biplane. structures.aero/blog/generating-aerodynamic-loads-hand-calculations-vs-aeroelasticity/
This is a great little tutorial. Maybe I should compare results to my own solver haha Sounds like a great company. If I'm ever planning to go to DC I'll definitely apply for open positions.
Great video! But how can I properly select structural nodes in order to have a spline that correclty transfer aero model to strucutral model? Which nodes should I choose?
m trying to practice this rigid trim and rigid trim off and m facing the same problem u did mention. even when m editing the trim card as suggested by you. whenever i recheck it, just to confirm that 1 against pops up. and my results are also the same. means rigid trim.onnd off deformationis exactly the same. please can you help me wirh how did manage tomitigate it
been able to do the analysis finally, but still unable to get the flutter animation for velocity where damping becomes positive, can u please help me with that. flutter preview thingie u mentioned is not working please
Aeroelasticity vs. Hand Calculations: Read our in-depth case study that covers generating aerodynamic loads for a Fokker Biplane. structures.aero/blog/generating-aerodynamic-loads-hand-calculations-vs-aeroelasticity/
Hi , could you please post the flutter velocity excel or question, in here?
thank you so much for the tutorial, its 4 years old but still helpful
Thanks for sharing your knowledge, from a french engineer student.
This is a great little tutorial. Maybe I should compare results to my own solver haha
Sounds like a great company. If I'm ever planning to go to DC I'll definitely apply for open positions.
Can we have the model to practice the analyses?
did you get the model?
Great video! But how can I properly select structural nodes in order to have a spline that correclty transfer aero model to strucutral model? Which nodes should I choose?
Hey Arthur
Did you get any solution to this? I am facing same issues.
Thanks
can we do Aeroelasticity in ANSYS software?
is there a way to generate Aero Panels which fit the wing surface?
Does this work for supersonic/hypersonic velocities? I don't see an option for using Piston theory anywhere.
Hey there. I need to perform similar simulation by not on aero body. Can i do it using these steps. My body is cantilevered tube in an air flow.
m trying to practice this rigid trim and rigid trim off and m facing the same problem u did mention. even when m editing the trim card as suggested by you. whenever i recheck it, just to confirm that 1 against pops up. and my results are also the same. means rigid trim.onnd off deformationis exactly the same. please can you help me wirh how did manage tomitigate it
been able to do the analysis finally, but still unable to get the flutter animation for velocity where damping becomes positive, can u please help me with that. flutter preview thingie u mentioned is not working please
I get this fatal error: "aeropanel area is zero", anyone knows why?
How can we import a CAD model into nastran