The Load Analysis and Aeroelastic Design department deals with issues that arise in the design of aircraft with regard to aeroelastic properties and aeroelastic requirements. Furthermore, developments ...
Figure 1: View of Global Finite Element Tug Model. Figure 2: Refined Structure in Way of Load Box. Figure 3: Load Application. Figure 4: ABS Load Box Yielding Evaluation Plot. Figure 5: Color Coded ...
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