A novel methodology for the robust preliminary design of rotorcraft is presented. The methodology is model-based
as opposed to empirically driven. A systems-engineering-inspired mindset is followed, manifesting in a hierarchical
approach to both design and modeling. The sources of uncertainty in a model-based design environment are discussed.
A concept to cope with these uncertainties in the context of preliminary design is presented. The hierarchical multi-
fidelity modeling strategy is depicted, after which the importance of a methodical and traceable model development
strategy across model fidelity levels is pointed out. A corresponding probabilistic approach is presented. A method
of merging these elements into a coherent methodology for robust preliminary design is outlined. A demonstration
of the developed methodology is subsequently conducted by applying this methodology to a fictive preliminary de-
sign problem. Ultimately, a discussion of the methodology is given based on the obtained results. The viability of
the methodology for quantifying and controlling the model-related uncertainty prevalent in model-based preliminary
design is successfully demonstrated.
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A novel methodology for the robust preliminary design of rotorcraft is presented. The methodology is model-based
as opposed to empirically driven. A systems-engineering-inspired mindset is followed, manifesting in a hierarchical
approach to both design and modeling. The sources of uncertainty in a model-based design environment are discussed.
A concept to cope with these uncertainties in the context of preliminary design is presented. The hierarchical multi-
fidelity modeling strategy is dep...
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