Lv31
250 积分 2025-01-08 加入
Turbulent atomisation of impinging jets under rising backpressure
1个月前
已完结
Effects of thermophoresis on high-pressure binary-species boundary layers with uniform and non-uniform compositions
4个月前
已关闭
Experimental Study of Low-Temperature Jet Injection Using Centrifugal Nozzles at Supercritical Pressure
5个月前
已完结
Numerical Study on Combustion and Atomization Characteristics of Coaxial Injectors for LOX/Methane Engine
5个月前
已完结
Flame dynamics of a subscale rocket combustor operating with gaseous methane and gaseous, subcritical or transcritical oxygen
5个月前
已关闭
Mascotte，a Research Test Facility for Cryogenic Combustion Research at High Pressure
5个月前
已关闭
Behaviors of Hypersonic Wing under Aerodynamic Heating
6个月前
已完结
Research on blending combustion characteristics of coaxial injector of oxygen/methane engine
6个月前
已完结
Research on blending combustion characteristics of coaxial injector of oxygen/methane engine
7个月前
已完结
An asymptotic theory formulating the surface ablation impact on Mack modes in high-enthalpy hypersonic boundary layers
10个月前
已完结
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