摘要简要介绍了高超声速飞行器动力系统的概况. 第2 部分介绍了超燃冲压发动机,
爆震发动机和组合循环发动机等典型高超声速吸气式发动机的基本工作原理与系统组成 …

Surrogate fuels are often used in place of real fuels in computational combustion studies.
However, many different choices of hydrocarbons to make up surrogate mixtures have been …

A comprehensive framework is proposed for Life Cycle Assessment (LCA) in the field of
commercial aviation (passengers and cargo), capable to ensure transparency and …

For the Computational Fluid Dynamics (CFD) modeling of combustion and detonation of Jet
A aviation fuel it is necessary to use the simplest kinetic mechanism that accurately …

Autoignition delay experiments in air have been performed in an atmospheric flow reactor
using typical natural gas components, namely, methane, ethane, and propane. Autoignition …

对航空煤油和单组份碳氢燃料正癸烷的雾化性能进行实验测试, 研究在部件燃烧特性验证阶段,
正癸烷作为航空煤油雾化过程代理燃料的可行性. 结果表明: 在室温条件下 …

Although the effects of microgravity, earth gravity, and hypergravity (> 1.5 g) on pool boiling
heat flux have been studied previously, pool boiling heat flux data over a continuous range …

Organophosphorus compounds (OPCs) are known to be combustion inhibitors (CI), fire
suppressants, or flame retardant molecules (FRMs) for polymers and as surrogates …

Ignition delay times of a “real” synthetic jet fuel (S8) were measured using an atmospheric
pressure flow reactor facility. Experiments were performed between 900 K and 1200 K at …

Atomization characteristics of aviation kerosene RP-3 and single component hydrocarbon
fuel n-decane were tested to study the feasibility of n-decane as an atomization surrogate …