Integrated aerodynamic and stealth optimization of aircraft based on NS/CFIE adjoint equations

被引：0
|
作者：
Huang J. [1 ]
Zhou L. [1 ]
Chen X. [1 ]
Ma C. [1 ]
Liu G. [1 ]
Gao Z. [2 ]
机构：
[1] Aerospace Technology Institute, China Aerodynamics Research and Development Center, Mianyang
[2] School of Aeronautics, Northwest Polytechnic University, Xi’an
来源：
Hangkong Xuebao/Acta Aeronautica et Astronautica Sinica | 2023年 / 44卷 / 12期
关键词：
aircraft; electromagnetic adjoint equation; flow adjoint equation; integration of aerodynamics and stealth; multidisciplinary coupled adjoint equation;
D O I：
10.7527/S1000-6893.2022.27757
中图分类号：
学科分类号：
摘要：
Advanced integrated aerodynamic and stealth design technology is the key link to realize the technical indexes of future combat aircraft，such as high stealth，high maneuverability，wide speed range and long range. This study derives the“coupled”adjoint equation of aerodynamic stealth based on the idea of interdisciplinary coupling adjoint. First，the adjoint equation of the flow field is constructed based on the Navier-Stokes equation. Through the variational processing of near-field vector multiplication，far-field vector multiplication，and the radar scattering area，the adjoint equation based on MLFMA is then developed. The electromagnetic adjoint equation of the algorithm，combined with the independently developed XSQP optimization framework and parametric modeling technology，constructs a highly reliable aerodynamic stealth comprehensive optimization technology platform. Taking a certain flying wing layout as the research object，we conduct the aerodynamic stealth integration test. The test results show that both the gradient calculation accuracy of the established accompanying platform and the optimization design efficiency are high，providing strong technical support for the aerodynamic stealth integration design of combat aircraft. © 2023 AAAS Press of Chinese Society of Aeronautics and Astronautics. All rights reserved.
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