The flow inside the aviation engine fire extinguishing system is complicated due to its
transient, two-phase and compressible nature. Temperature is one of the important variables …

The fire-extinguishing system is an indispensable fire-protection facility on the aircraft. In
order to guide weight reduction of the aircraft's fixed gas fire-extinguishing system by …

The aim of this work is to provide a formulation of a non-linear diffusion model in the form of
a Porous Medium Equation (PME) with application to a fire extinguishing process in an …

Reducing the release pressure of fire extinguishing systems can decrease potential safety
hazards in large transport airplanes. To explore whether reducing the release pressure can …

In order to guide the optimization design of the nozzle of the aircraft-fixed gas fire
extinguishing system, we studied the influence of nozzle geometric parameters including …

To provide guidance towards reducing the weight of the HFC-125 storage vessel by
reducing the release pressure and to reveal the effects of release pressure on the …

In order to guide the optimization design of the pipeline network of the aircraft-fixed gas fire
extinguishing system and improve its fire extinguishing performance, FLUENT software was …

The static method of isochoric saturation was used to measure the solubilities of CO2, O2
and N2 in rocket propellant 5 (RP5) at temperatures ranging from 253.15 to 323.15 K in 10 K …

提出了无人机油箱地面洗涤惰化技术理论和方法, 利用CFD 方法研究了采用地面洗涤惰化技术
降低油箱气相空间氧体积分数并使无人机油箱在地面和飞行条件下仍然保持惰化状态的可行性 …

In this study, the injection of Halon 1301, an effective fire-suppressing agent, into a
helicopter engine nacelle is modelled to provide insights into dispersion behaviour …