The results show that,micro flow near a wall reduces capillary pressure gradient and liquid superheat as well as increasing solid-liquid interfacial thermal resistance,worsening liquid film spreading and heat transfer characteristics,effects of which are not to be neglected in the evaporating thin film region.

Taking the measured data of the power plant as the inputs of the model, average wall heat flux, drum pressure and steam mass flow rate in the outlet of the system are calculated; by the drives of some typical pertur.

Numerical simulation of combustion in a wall jet combustor;

38mm) and impingement wall surface curvature (semi-cylinder diameter D = 150mm) on impingement wall jet flow and its turbulent structure are presented.

Study and numerical calculation wall streamline distributions for hypersonic vehicle according to Euler equation;