JB
Jasper Bussemaker
2 records found
1
Authored
Wing Optimization with Active Load Control
Integrating Maneuver Load Control and Gust Load Alleviation in Wing Structural Optimization of Large Transport Aircraft
Improving the performance of large transport aircraft requires high aspect ratio and lightweight wings, making aeroelasticity an important factor in wing structural design. Active control of aeroelastic loads can be used to improve the aeroelastic behavior of the wing.
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Contributed
Aircraft Jet Engine Architecture Modeling
Creating a Benchmark Problem using a System Architecting Approach with Mixed-Discrete & Multi-Objective Capabilities
With an increasing complexity of systems, systematic design space exploration is required for fair analysis and comparison of architecture design options. However, there is still a need for a benchmark problem to support the development & evaluation of optimization algorithms
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