Chaoyang Liu

Design and multi-objective optimization approach for the waverider based on deep neural operators

Zhentao Zhao, Xi He, Hao Wang, Kefeng Deng et autres

cn (code pays fourni par la source)

Analysis of similarity criteria for jet flow under low-altitude high-speed conditions based on wind tunnel experiment

Zan Xie, Shi-bin Li, Chaoyang Liu, Yaobin Niu et autres

cn (code pays fourni par la source)

Numerical investigation of aluminum powder combustion with upstream kerosene auxiliary burner in a supersonic cavity-based combustor

Wenxiong Xi, Liteng Yao, Linhong Li, Jian Liu et autres

cn, se (code pays fourni par la source)

Vortices-controlled mixing and combustion enhancement in a supersonic cavity-stabilized combustor by herringbone micro-ribs

Junbo Zou, Yu Pan, Chaoyang Liu, Xin Li

cn (code pays fourni par la source)

Study on wind tunnel experiment and numerical simulation of the aerospike-jet composite drag reduction approach in high-speed freestream

Zan Xie, Jian Zhao, Chaoyang Liu, Wei Huang

cn (code pays fourni par la source)

Research Status on the Mixing Mechanism and Enhancement of Supersonic Gas-Liquid Transverse Jet Mixer

Zihao Li, Chaoyang Liu, Yi-xuan Tao, Wei Huang

As the core technology for fuel mixing in scramjet engines, supersonic transverse jets play a crucial role. The complexity of their flow structure and mixing efficiency directly determine the engine’s performance, presenting a key bottleneck in the development of near - space …

cn (code pays fourni par la source)

Investigation on combustion characteristics of three novel strut-based combustors using OpenFOAM

Zi-jian Zhao, Chaoyang Liu, Wei Huang

cn (code pays fourni par la source)

Aerodynamic drag analysis in hypersonic jet-induced flowfields using similarity criteria

Zan Xie, Shi-bin Li, Ya-jie Liang, Chaoyang Liu et autres

Based on jet momentum similarity, the applicability of conventional hypersonic wind tunnels operating at a freestream total pressure of 2 MPa and total temperatures ranging from 500 K to 900 K was investigated for simulating jet interaction flowfield aerodynamic drag under representative …

cn (code pays fourni par la source)

A preliminary study of drag reduction mechanism via the aerospike-jet composite approach in low-altitude high-speed flow regimes

Zan Xie, Chaoyang Liu, Yu-shan Meng, Wei Huang et autres

cn (code pays fourni par la source)

Large eddy simulation of fuel/air co-flow jet mixing enhancement in supersonic crossflow

Xin Li, Yu Pan, Chaoyang Liu, Junbo Zou

cn (code pays fourni par la source)

Enhancing mixing and combustion using Chevron riblets in near-wall jet injection into supersonic flows

Junbo Zou, Yu Pan, Chaoyang Liu, Xin Li

Chevron riblets leverage their unique geometric configuration to induce abundant vortical structures, enhancing turbulent characteristics of the flow field and effectively enhancing fuel−oxidizer mixing and combustion. This study integrates Chevron riblets into the Burrows−Kurkov supersonic near-wall jet combustion. A large-eddy simulation approach …

cn (code pays fourni par la source)

Numerical investigation on the characteristics of the near-wall jet combustion in the supersonic turbulent flows

Junbo Zou, Yu Cheng Pan, Chaoyang Liu, Xin Li et autres

cn (code pays fourni par la source)