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Inverse design framework for optimizing solid propellant grains toward target performance profiles

delete2025-09-17
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PRE
AI
E
Euiyoung Kim
S
Seongpil Joo
S
Sahuck Oh *
DOI:10.1016/j.actaastro.2025.09.039delete
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摘要

摘要

En 中文
• 提出了一种固体推进剂药柱优化的逆向设计框架。 • 该方法识别满足性能要求的药柱构型。 • 算例验证了所提出方法的有效性。 • 该框架促进了推进系统设计的系统性开发。
Keyword:
Solid rocket motor
Artificial neural network
Genetic algorithm
Shape optimization
Burnback analysis

期刊

Acta Astronautica 封面图
Acta Astronautica
IF:
3.4
论文数:
1.2W
被引数:
2.1W

机构

K
Korea Aerospace University
学者数:
1.1K
论文数: 1.1K
被引数: 513
A
Agency for Defense Development
学者数:
129
论文数: 65
被引数: 975
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