A Combined Artificial-Intelligence Aerodynamic Design Method for a Transonic Compressor Rotor Based on Reinforcement Learning and Genetic Algorithm
نویسندگان
چکیده
An aircraft engine’s performance depends largely on the compressors’ aerodynamic design, which aims to achieve higher stage pressure, efficiency, and an acceptable stall margin. Existing design methods require substantial prior knowledge different optimization algorithms determine 2D 3D features of blades, in policy needs be more readily systematized. With development artificial intelligence (AI), deep reinforcement learning (RL) has been successfully applied complex problems domains provides a feasible method for compressor design. In addition, applications AI research have progressively developed. This paper described combined artificial-intelligence based modified deterministic gradient algorithm genetic (GA) integrated GA into RL framework. The trained agent learned used it improve result single-stage transonic rotor. Consequently, rotor exhibited pressure ratio efficiency owing sweep feature, lean airfoil angle changes. separation near tip secondary flow decreased after process, at same time, shockwave was weakened, providing improved efficiency. Most these beneficial field remained modification ratio, showing that by generally universal. combination other is expected benefit future designs merging advantages methods.
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ژورنال
عنوان ژورنال: Applied sciences
سال: 2023
ISSN: ['2076-3417']
DOI: https://doi.org/10.3390/app13021026