GENERAL VARIATIONAL PRINCIPLE FAMILY FOR FULLY 3-D UNSTEADY TRANSONIC FLOW WITH SHOCKS AROUND OSCILLATING WINGS  

GENERAL VARIATIONAL PRINCIPLE FAMILY FOR FULLY 3-D UNSTEADY TRANSONIC FLOW WITH SHOCKS AROUND OSCILLATING WINGS

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作  者:刘高联 

机构地区:[1]Shanghai Institute of Mechanical Engineering

出  处:《Science China Mathematics》1989年第6期707-715,共9页中国科学:数学(英文版)

摘  要:Based on the author’s previous work, a general form of generalized variational princi-ples (VPs) together with its derived VP family is established for 3-D unsteady’ transonicpotential flow with shocks past arbitrary wings oscillating periodically. To facilitate thenumerical handling, full use is made of functional variations with variable domain and natu-ral boundary conditions (BC) so that almost all boundary/interface conditions, including theRankine-Hugoniot shock relations and slip conditions across free trailing vortex sheets, havebeen converted into natural ones. Also distributed suction/blowing along the wing surfacefor the boundary layer control is accounted for. This theory aims at rendering a general,rigorous theoretical basis for the finite element metbod and other direct variational methods,and it can be generalized to both wing-body combinations and 3-D rotating bladings, includ-ing the subsonic flow as a special case.Based on the author's previous work, a general form of generalized variational princi-ples (VPs) together with its derived VP family is established for 3-D unsteady' transonicpotential flow with shocks past arbitrary wings oscillating periodically. To facilitate thenumerical handling, full use is made of functional variations with variable domain and natu-ral boundary conditions (BC) so that almost all boundary/interface conditions, including theRankine-Hugoniot shock relations and slip conditions across free trailing vortex sheets, havebeen converted into natural ones. Also distributed suction/blowing along the wing surfacefor the boundary layer control is accounted for. This theory aims at rendering a general,rigorous theoretical basis for the finite element metbod and other direct variational methods,and it can be generalized to both wing-body combinations and 3-D rotating bladings, includ-ing the subsonic flow as a special case.

关 键 词:variational principles in fluid mechanics UNSTEADY FLOW finite element method TRANSONIC flow. 

分 类 号:N[自然科学总论]

 

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