This is particularly interesting since the implemented load alleviation functions are designed to reduce loads, and not explicitly to improve passenger ride comfort. To address this issue, the DLR MONA based design and the TUB flight mechanical assessment tool MITRA are linked to investigate the impact of the structural design on specific flight mechanical assessments such as passenger ride comfort. Current available tools and methods are not accurate enough for this task. For an efficient design process, it is essential to answer such questions with accurate multi-disciplinary tools and methods as early as possible to minimize development risk and avoid costly and time-consuming redesign loops. For example, it is important to know how at that design stage such flexible aircraft with load alleviation affect passenger ride comfort in turbulent flight. At the same time, the structural design impacts other disciplines in preliminary aircraft design, especially flight mechanics. ![]() Additionally, load alleviation functions are implemented to reduce the structural loads, which results in further reductions of the structural stiffness. ![]() Consequently, those aircraft are more flexible. ![]() New fuel-efficient aircraft designs have high aspect ratio wings.
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