A study of morphing aircraft on morphing rules along trajectory

نویسندگان

چکیده

Morphing aircraft can meet requirements of multi-mission during the whole flight due to changing aerodynamic shape, so it is necessary study its morphing rules along trajectory. However, trajectory planning considering variables requires a huge number expensive CFD computations in view performance. Under given missions and trajectory, alleviate computational cost improve trajectory-planning efficiency for aircraft, an offline optimization method proposed based on Multi-Fidelity Kriging (MFK) modeling. The angle attack, Mach number, sweep axial position wing are defined as generating training data building MFK models, which many inviscid solutions used low-fidelity data, while less high-fidelity obtained by solving viscous flow. Then built models lift, drag pressure centre at different angles attack numbers predict performance keeps optimal planning. Hence, be correspondingly acquired well keep with best task. was performed only using 240 110 data. results indicate that complex take advantage keeping good performance, more efficient than reducing 86% computing time.

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ژورنال

عنوان ژورنال: Chinese Journal of Aeronautics

سال: 2021

ISSN: ['1000-9361', '2588-9230']

DOI: https://doi.org/10.1016/j.cja.2020.04.032