Inputs of the Doublet Lattice Method are the mode shapes, as far as the translational displacement components are concerned. Actually, the doublet lattice code needs the equation of the shape so that the slopes can be effectively calculated and the fluid-structure boundary condition can be imposed. These tasks are achieved with the splining, which is discussed in this chapter.
From the Structural Mesh to the Aerodynamic Mesh: Splining
Introduction to Unsteady Aerodynamics and Dynamic Aeroelasticity ; Kapitel : 29 ; 521-547
11.06.2024
27 pages
Aufsatz/Kapitel (Buch)
Elektronische Ressource
Englisch
Aerodynamic mesh , Infinite Plate Spline Method , Control point , Aerodynamic influence coefficient matrix in structural degrees of freedom , Structural mesh , Load point , Mode Mechanical Engineering , Physics and Astronomy , Structural Materials , Mechanical Statics and Structures , Aerospace Technology and Astronautics , Engineering
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