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 ...

The computation of flight and ground loads acting on the aircraft structure is one of the main tasks in the design and certification process of an aircraft. The term loads comprises all steady and ...

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 ...

Distributed power architectures for advanced system designs have evolved to the point where cost-performance optimization is sensitive to the choice and location of load bypass capacitors. Over the ...

In load pull calculations, power amplifiers are going to need harmonic load pull analysis and load pull contours with wideband electromagnetic tuners. Working with RFIC power amplifiers is difficult ...