Abstract
An aerodynamic configuration of a supersonic business jet wing-body is proposed as baseline for a robust aerodynamic shape design problem. This configuration has been analyzed to identify the main dependencies and interactions of the parameters that describe the uncertainty sources in the robust design problem. Subsequent steps of the research activity will be related to the robust natural laminar flow design optimization of this configuration.
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Quagliarella, D., Iuliano, E. (2019). Uncertainty Sources in the Baseline Configuration for Robust Design of a Supersonic Natural Laminar Flow Wing-Body. In: Minisci, E., Vasile, M., Periaux, J., Gauger, N., Giannakoglou, K., Quagliarella, D. (eds) Advances in Evolutionary and Deterministic Methods for Design, Optimization and Control in Engineering and Sciences. Computational Methods in Applied Sciences, vol 48. Springer, Cham. https://doi.org/10.1007/978-3-319-89988-6_22
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DOI: https://doi.org/10.1007/978-3-319-89988-6_22
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