Paper
16 August 2024 Optimal design of supersonic inlet considering uncertainty
Author Affiliations +
Proceedings Volume 13218, First Aerospace Frontiers Conference (AFC 2024); 132180C (2024) https://doi.org/10.1117/12.3032420
Event: First Aerospace Frontiers Conference (AFC 2024), 2024, Xi’an, China
Abstract
The inlet performance of an air-breathing aircraft plays a key role in its cruise flight. The uncertainty and random disturbances in inflow conditions pose a challenge to the inlet performance. This paper conducts research on the optimal design of the supersonic inlet taking into account the uncertainty of the inflow to improve the robustness of the inlet performance. The polynomial chaos expansion method is used to conduct uncertainty analysis, and the expansion coefficient is obtained through the sparse grid point allocation method. Sensitivity analysis of the inflow uncertainty parameters is further conducted to determine the key influencing parameters. Finally, combined with uncertainty analysis and gradient-based optimization method, the supersonic inlet is optimized considering uncertainty. The results show that under the condition of inflow disturbance, in order to meet the flow requirements of the engine, the capture area of the uncertainty optimal design is larger than that of the deterministic optimal design. The optimization design method considering uncertainty can effectively improve the robustness of the inlet performance.
(2024) Published by SPIE. Downloading of the abstract is permitted for personal use only.
Hai Fang, Suyun Liu, Xiaobing Shang, Xu Duan, and Shenming Quan "Optimal design of supersonic inlet considering uncertainty", Proc. SPIE 13218, First Aerospace Frontiers Conference (AFC 2024), 132180C (16 August 2024); https://doi.org/10.1117/12.3032420
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KEYWORDS
Design

Chaos

Uncertainty analysis

Mathematical optimization

Aerodynamics

Engineering

Computer programming

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