Three issues on nozzle thrust performance in cold-to-hot correlation considering variable specific heat effect von Chen, Kuangshi, Xu, Jinglei, Qin, Qihao, Song, Guangtao

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Numerical study of a trapezoidal bypass dual throat nozzle von HUANG, Shuai, XU, Jinglei, YU, Kaikai, WANG, Yangsheng, PAN, Ruifeng, CHEN, Kuangshi, ZHANG, Yuqi

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Application of Boundary Layer Combustion in High-Mach-Number Scramjets von Peng, Yuan, Xu, Jinglei, Chen, Kuangshi

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Analytical solution of supersonic axisymmetric flow around a sharp convex corner von Chen, Kuangshi, Xu, Jinglei, Qin, Qihao, Huang, Shuai

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Design of Thrust-Optimized Scramjet Nozzle and Its Concise Estimation Method von Chen, Kuangshi, Xu, Jinglei, Qin, Qihao, Xiong, Weijian

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Numerical investigation of the shock-focusing detonation engines with different nozzle configurations von Li, Rui, Xu, Jinglei, Lv, Haiyin, Yu, Kaikai, Chen, Kuangshi

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Suppression and utilisation of aeroelastic behaviour in turbine-based combined cycle inlet von Qin, Qihao, Xu, Jinglei, Chen, Kuangshi

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Modular design framework of an axisymmetric wrap-around thrust-optimized combined nozzle von Chen, Kuangshi, Xu, Jinglei, Qin, Qihao, Li, Rui, Yu, Kaikai

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Living cell DNA marker signal amplification method based on CRISPR/dCas9 system and oligonucleotide probe von CHEN KUANGSHI, MAO SHIQI

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Living cell single-molecule RNA (Ribonucleic Acid) labeling method based on fluorescence resonance energy transfer von CHEN KUANGSHI, MAO SHIQI

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Throat offset fluidic thurst vectoring nozzle having asymmetric backbody profile von HUANG, Shuai, CHEN, Kuangshi, XU, Jinglei, WANG, Feng, WANG, Yangsheng, JIANG, Jingjing

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Throat offset pneumatic vector nozzle having asymmetric rear body profile von HUANG, Shuai, CHEN, Kuangshi, XU, Jinglei, WANG, Feng, WANG, Yangsheng, JIANG, Jingjing

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Hypersonic thrust vectoring nozzle and translation adjustment and flow control method thereof von WEI LIXIANG, XU JINGLEI, HUANG SHUAI, CHEN KUANGSHI

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Hypersonic thrust vectoring nozzle and sliding adjustment method thereof von WEI LIXIANG, XU JINGLEI, HUANG SHUAI, CHEN KUANGSHI

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Design method for variable-geometry asymmetric spray pipe of coupling rocket thrust chamber von XU JINGLEI, HUANG SHUAI, QIAO MINGKUN, CHEN KUANGSHI

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A THROAT SHIFTING TYPE FLUIDIC VECTORING NOZZLE BASED ON TRANSLATIONAL MOTION FOR SHORT-DISTANCE TAKEOFF AND LANDING von XU, JINGLEI, HUANG, SHUAI, WANG, YANGSHENG, LIN, YONGCHEN, CHEN, KUANGSHI, XU, BAOCHENG, WANG, FENG

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Throat offset pneumatic vector nozzle having asymmetric rear body profile von HUANG, Shuai, CHEN, Kuangshi, XU, Jinglei, WANG, Feng, WANG, Yangsheng, JIANG, Jingjing

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Multi-channel maximum thrust combined nozzle design method based on supersonic shear layer modeling and supersonic shear layer modeling algorithm von XU JINGLEI, HUANG SHUAI, ZHOU JIANXING, CHEN KUANGSHI

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Pneumatic thrust vectoring nozzle and control method thereof von LAN JIAZHE, ZHANG YUQI, HUANG SHUAI, XU JINGLEI, SONG GUANGTAO, PAN RUIFENG, CHEN KUANGSHI

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Mechanical disturbance type thrust vectoring nozzle and expansion section wall surface design method von ZHANG YUQI, HUANG SHUAI, XU JINGLEI, SONG GUANGTAO, PAN RUIFENG, CHEN KUANGSHI

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