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Introduction to Aeroelasticity in Nastran (NX Nastran with Femap)

  Рет қаралды 33,202

Structural Design and Analysis, Inc.

Structural Design and Analysis, Inc.

Күн бұрын

Watch part 2 of our aeroelasticity series where we cover aeroelastic analysis of a full aircraft: structures.aer...
Subscribe to our channel: / @structuraldesignanaly...
Structural Design and Analysis (Structures.Aero) is a structural analysis company that specializes in aircraft and spacecraft structures using composites.
We utilize Femap, NX Nastran, Fibersim, Simcenter 3D, and HyperSizer in our analysis work and provide these programs, training, and support as a Value-Added Reseller for Siemens PLM and HyperSizer.
CONNECT WITH US
Join the Femap/NX Nastran User Group: / 232625983920053
Facebook: / structuraldesignandana...
Twitter: / structuresaero
LinkedIn: / structural-design-and-...

Пікірлер: 25
@StructuralDesignAnalysisInc
@StructuralDesignAnalysisInc 7 жыл бұрын
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/
@nelon5933
@nelon5933 3 жыл бұрын
Hi , could you please post the flutter velocity excel or question, in here?
@clementf.8256
@clementf.8256 4 жыл бұрын
Thanks for sharing your knowledge, from a french engineer student.
@cityblue7029
@cityblue7029 3 жыл бұрын
thank you so much for the tutorial, its 4 years old but still helpful
@arthurbarreto8220
@arthurbarreto8220 3 жыл бұрын
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?
@muhammadumerfarooq9459
@muhammadumerfarooq9459 Жыл бұрын
Hey Arthur Did you get any solution to this? I am facing same issues. Thanks
@rafaelguedes5093
@rafaelguedes5093 6 жыл бұрын
Can we have the model to practice the analyses?
@johnblahbah5150
@johnblahbah5150 3 жыл бұрын
did you get the model?
@TennisGvy
@TennisGvy 6 жыл бұрын
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.
@gabrielelausdei3146
@gabrielelausdei3146 5 ай бұрын
is there a way to generate Aero Panels which fit the wing surface?
@nareshjonna11
@nareshjonna11 5 жыл бұрын
can we do Aeroelasticity in ANSYS software?
@larsjansen4245
@larsjansen4245 6 ай бұрын
Does this work for supersonic/hypersonic velocities? I don't see an option for using Piston theory anywhere.
@muhammadumerfarooq9459
@muhammadumerfarooq9459 Жыл бұрын
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.
@ehsanahmad7169
@ehsanahmad7169 2 жыл бұрын
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
@ehsanahmad7169
@ehsanahmad7169 2 жыл бұрын
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
@viharize
@viharize 3 жыл бұрын
How can we import a CAD model into nastran
@alessandrok.4798
@alessandrok.4798 3 жыл бұрын
I get this fatal error: "aeropanel area is zero", anyone knows why?
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