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 ; Chapter : 29 ; 521-547
2024-06-11
27 pages
Article/Chapter (Book)
Electronic Resource
English
Aerodynamic mesh , Structural mesh , Mode , Infinite Plate Spline Method , Control point , Load point , Aerodynamic influence coefficient matrix in structural degrees of freedom Engineering , Aerospace Technology and Astronautics , Mechanical Engineering , Mechanical Statics and Structures , Structural Materials , Physics and Astronomy
Staggered-Mesh Computation for Aerodynamic Sound
AIAA | 2000
|Staggered-mesh computation for aerodynamic sound
AIAA | 1998
|Automatic mesh generation for vehicle aerodynamic analysis
Tema Archive | 1998
|