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Numerical Simulation of Cavitation and Ventilation Phenomena During Aircraft Ditching
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作者 CHEN Xingyi LI Meng +2 位作者 TONG Mingbo WU Bin ZHANG Xianzheng 《Transactions of Nanjing University of Aeronautics and Astronautics》 EI CSCD 2022年第S01期9-15,共7页
The large eddy simulation(LES)method combined with the global dynamic grid strategy is used to numerically study the influence of pitch angles on cavitation and ventilation phenomena in the rear of fuselage during dit... The large eddy simulation(LES)method combined with the global dynamic grid strategy is used to numerically study the influence of pitch angles on cavitation and ventilation phenomena in the rear of fuselage during ditching.The volume of fluid(VOF)method is used to capture the interface.By analyzing the normal force,moment,pressure distribution and nephograms,we find that the pitch angle has a great influence on the total load,the cavitation occurrence time and its transition to ventilation,thus affects the longitudinal load distribution and the controlling of aircraft dynamics. 展开更多
关键词 aircraft ditching CAVITATION large eddy simulation(LES) ventilation volume of fluid(VOF)
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