Numerical simulation of flow transition in microchannel

Pressure drop characteristics of supercritical aviation kerosene in U-turn tube

Heat transfer characteristics in an internal coolant passage with crossflow-induced swirl, impingement and film cooling holes

Data processing of blade's transient heat transfer experiment in short duration wind tunnel

Experiment on the effects of side load and pipe diameter on the characteristics of boiling two-phase pipe flow

National Key Laboratory of Science and Technology on Aero-Engine Aero-Thermodynamics,School of Energy and Power Engineering,Beijing University of Aeronautics and Astronautics

School of Jet Propulsion, Beijing University Aeronautics and Astronautics

School of Power and Energy,Northwestern Polytechnical University

南京航空航天大学航空学院飞行器环境控制与生命保障工业和信息化重点实验室

中国航空工业集团有限公司金城南京机电液压工程研究中心航空机电系统综合航空科技重点实验室