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Integration of Low-Fidelity MDO and CFD-Based Redesign of Low-Boom Supersonic Transports

2021; American Institute of Aeronautics and Astronautics; Volume: 59; Issue: 10 Linguagem: Inglês

10.2514/1.j060368

1533-385X

Wu Li, Karl Geiselhart,

Aerospace and Aviation Technology

A mixed-fidelity low-boom multidisciplinary optimization (MDO) problem is formulated for integration of low-fidelity MDO and computational fluid dynamics (CFD)-based low-boom inverse design optimization. The mixed-fidelity low-boom MDO problem aims to enforce the weight consistency for CFD-based low-boom inverse design optimization: the optimum low-boom configuration is designed for the weight at the start of cruise of the same configuration for the low-boom overland mission. Moreover, it also seeks the optimum trades between the maximum takeoff gross weight (MTOGW), cruise Mach, and range for the low-boom overland mission while meeting the requirement of flying a transatlantic overwater mission. A block coordinate optimization (BCO) method is developed to find an approximate solution of the mixed-fidelity low-boom MDO problem. The BCO method is successfully applied to generate two CFD-based low-boom configurations that closely match two reversed equivalent area targets with ground noise levels below 70 PLdB, respectively. Moreover, these CFD-based low-boom configurations can be obtained with minor wing modifications from the solutions of the low-fidelity MDO problem. The low-fidelity MDO solutions are Pareto points for constrained multi-objective optimization of MTOGW, low-boom cruise Mach, and low-boom range. The best low-fidelity MDO concept flies at cruise Mach 1.8 for a low-boom overland mission with range of 2950 nm and an overwater mission with range of 3600 nm.