.

Changjian Zhao1, Feng Yang1,2, Xiaohui Wang3

  • 1China Academy of Launch Vehicle Technology, Beijing 100076, China.

概括

这项研究开发了一种用于高温空气动力学疲劳测试航空发动机外的模型. 优化的系统设计确保了精确的疲劳负载控制,提高了航空发动机的可靠性.

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