Print Email Facebook Twitter Panel methods in aerodynamics: Some highlights Title Panel methods in aerodynamics: Some highlights Author Hoeijmakers, H.W.M. Institution National Aerospace Laboratory NLR Date 1987-03-20 Abstract A survey Is presented of several aspects of the use and further development of panel methods in aerodynamics. Aspects discussed include possible types of boundary conditions, low versus higher-order formulations, simulation of subsonic and supersonic flow and modeling of wakes as well as of leading-edge vortex separation. Also discussed are computational aspects of panel methods and possible directions for new developments. The latter include the extension of the domain of applicability to compressible flow and the coupling with viscous flow methods, as well as ways to improve the efficiency of the panel method. Invited lecture presented at Third Gamm-Semlnar Kiel "PANEL METHODS IN MECHANICS", Kiel, West-Germany, January 16-18, 1987. To reference this document use: http://resolver.tudelft.nl/uuid:d1ee1b5d-f312-42fc-9224-1446eaf2cf75 Publisher Nationaal Lucht- en Ruimtevaartlaboratorium Access restriction Campus only Source NLR MP 87028 U Part of collection Aerospace Engineering Reports Document type report Rights (c) 1987 National Aerospace Laboratory NLR Files PDF 87028.pdf 26.48 MB Close viewer /islandora/object/uuid:d1ee1b5d-f312-42fc-9224-1446eaf2cf75/datastream/OBJ/view