the Aviation Science Foundation of China(No.20151067003)。
In order to improve the accuracy of damage region division and eliminate the interference of damage adjacent region,the airframe damage region division method based on the structure tensor dynamic operator is proposed...
This research work is supported by the National Science and Technology Major Project(2017-V-0004-0054);the National Natural Science Foundation of China(Grant No.52125603);the National Natural Science Foundation of China(Grant No.11972139);the Fundamental Research Funds for the Central Universities(HIT.BRET.2021006 and FRFCU5710094620).
Airbreathing aero-engines are regarded as excellent propulsion devices from ground takeoff to hypersonic flight,and require control systems to ensure their efficient and safe operation.Therefore,the present paper aims...
supported by the Aeronautical Science Foundation of China(No.20151067003)。
In order to obtain the image of airframe damage region and provide the input data for aircraft intelligent maintenance,a multi-dimensional and multi-threshold airframe damage region division method based on correlatio...
supported by Youth Science and Technology Research Fund;Shanxi Province Applied Basic Research Projectgrant number 201801D221039;Science Foundation of North University of China grant number XJJ201813;Scientific and Technologial Innovation Programs of Higher Education Institutions in Shanxi grant number 2019L0570;Aeronautical Science Foundation of China grant number 2019020U0002。
A hypersonic aerodynamics analysis of an electromagnetic gun(EM gun) launched projectile configuration is undertaken in order to ameliorate the basic aerodynamic characteristics in comparison with the regular projecti...
supported by the Fundamental Research Funds for the Central Universities (Nos. 3102019JC009 and G2016KY0002)
Civil aviation faces great challenges because of its robust projected future growth and potential adverse environmental effects. The classical Tube-And-Wing(TAW) configuration following the Cayley’s design principles...
supported by the Fundamental Research Funds for the Central Universities (Nos. 3102019JC009 and G2016KY0002)
Strong shock waves and flow separation often occur during the integration of nacelle and airframe for blended-wing-bodies with podded engines. To address this problem, this paper presents an integration method with nu...
Fundamental features of aerodynamic interference and integration of airframes and air-breathing jet engines for high-speed flight vehicles are studied within the framework of supersonic small perturbation theory.Both ...
supported by UT-INSA Program(2013);the support of the China Scholarship Council(CSC)
Airframe maintenance is traditionally performed at scheduled maintenance stops.The decision to repair a fuselage panel is based on a fixed crack size threshold,which allows to ensure the aircraft safety until the next...
supported by the National Basic Research Program of China (No.2014CB744800)
With the progress of high-bypass turbofan and the innovation of silencing nacelle in engine noise reduction, airframe noise has now become another important sound source besides the engine noise. Thus, reducing airfra...