ITO thin film thermocouple for dynamic inner wall temperature measurement of supersonic combustion. - Xinhang Jin; Binghe Ma; Tao Qiu; Jinjun Deng; Jian Luo 008; Weizheng Yuan; Jialing Le; Yiyu Han (IEEE SENSORS, 2017)

Supersonic combustion flow field reconstruction based on multi-view domain adaptation generative network in scramjet combustor. - Mingming Guo; Erda Chen; Ye Tian; Linjing Li; Mengqi Xu; Jialing Le; Hua Zhang (Eng. Appl. Artif. Intell., 2024)

Supersonic combustion field evolution prediction in scramjet engine using a deblurring multi-scale attention network. - Erda Chen; Mingming Guo; Jiawen Deng; Ye Tian; Xue Deng; Jialing Le; Hua Zhang (Expert Syst. Appl., 2024)

Research on intelligent prediction method of supersonic flow field in scramjet based on deep learning: A review. - Xue Deng; Ye Tian; Erda Chen; Maotao Yang; Hua Zhang; Jialing Le (Expert Syst. Appl., 2025)

Time-space adaptive implicit-explicit method for unsteady detonations. - Xuke Zhang; Bin Zhang; Wei Zhong; Jialing Le (J. Comput. Phys., 2025)

Hybrid physics-machine learning framework for mathematical modeling of supersonic combustion mode transitions across wide speed range. - Zhiwen Zhong; Ye Tian; Wenyan Song; Jialing Le (Knowl. Based Syst., 2025)