Simulating the high-pressure common-rail fuel injection system of diesel engines;

Intelligent update and design of a fuel injection system test device;

Design and Experimental Research of Fuel Injection and Ignition Control System for Electronically Controlled Gasoline Engine;

The fluid model is set up according to some storing and transporting canister to study the jet flow during acci- dental ignition in this thesis.

The article calculates unsteady initial shock wave produced by jet flow in launcher.

During launching stage of rocket,the influence of jet flow on rectangular tube is a complex process,the distortion of the rectangular tube can be more obvious in the launching experiment.

Research on dynamic characteristics of underwater superasonic gas jets

In this paper, the time-dependent ignition process of gas jet for launch underwater was studied by means of numerical simulation.

This method is robust,and it offers a new means for numerical study of gas jet.

The exhaust jet in the exhaust channel of the vertical launching system(VLS) during a missile launches was researched using the numerical methods in this paper.