Aeroelastic analysis is performed on a parallel computer using Euler equations coupled with an advanced wing-box structural model. The wing-box consists of a 3-noded triangular element, with two inplane translations and an in-plane rotation at each node, and axial rods. The 9 degree of freedom triangular element provides more accurate stress analysis than previous studies. A typical wing-body configuration is chosen for the analysis with the assumption of a rigid body. Preliminary results are presented.
Parallel aeroelastic computation by using coupled Euler flow and wing-box structural models
Parallele Aeroelastizitätsberechnung unter Verwendung der Eulerschen Strömungsgleichungen, gekoppelt mit einem Flügelkasten-Strukturmodell
1995
3 Seiten, 6 Bilder, 9 Quellen
Conference paper
English
Parallel Aeroelastic Computations by Using Coupled Euler Flow and Wing-Box Structural Models
British Library Conference Proceedings | 1995
|British Library Conference Proceedings | 2002
|