The first topic to be covered will be how to set up an aeroelastic trim analysis on an entire aircraft, and how to interpret the results. This will include how to setup a control surface, apply appropriate support constraints, and apply incidence/twist angles to the wing aerodynamic surfaces.
Flutter Analysis
The second topic to be covered will be how to run a flutter analysis for an entire aircraft. We will touch on some of the differences between flutter analysis for an entire structure as opposed to a wing at a fixed boundary condition. Finally, we will explore body freedom flutter and identify some rules of thumb to indicate if this instability is likely to present itself within the flight envelope.
What is in this webinar? Siemens Principle Applications Engineer Chip Fricke will be presenting this webinar on Simcenter Nastran Solutions 401 & 402. Some of the topics covered will be: Overview of Simcenter Nastran Multi-step Nonlinear Solutions ...
What is in this webinar? In this webinar, we go behind the scenes on our work for the A3 Vahana project. We discuss how FEA can compliment and reduce time in the design process. Some ways FEA was used to reduce time: Modal analysis. Femap's mass ...
What is in this webinar? This webinar will demonstrate the use of advanced nonlinear and how to set up a few typical scenarios. NASTRAN Details and Licensing Advanced Support Services
What is in this webinar? In this webinar, Alex Skavdahl will explore post-buckled behavior by running a model far in excess of when it buckles. The advanced non-linear solver can track the post-buckled behavior well into the plastic range. It’s ...
What is in this webinar? This webinar will cover the following topics: Aeroelasticity overview Static aeroelastic example Aeroelastic tailoring Flutter example NASTRAN Details and Licensing Advanced Support Services