A computational fluid dynamics (CFDs) method utilizing unstructured grid technology has been employed to compute vortical\r\nflow around a 65? delta wing with sharp leading edge, which is specially known as the geometry of the second international vortex\r\nflow experiment (VFE-2). In VFE-2, 65? delta wings with different leading edges had been broadly investigated by experiments,\r\nwhich resulted in a special database for CFDs codes validation. The emphasis of this paper is to investigate the effectiveness of an\r\nadjoint-base grid adaptation method for unstructured grid in capturing concentrated vortices generated at sharp edges or flow\r\nseparation lines of lifting surfaces flying at high angles of attack. Earlier experiences in vortical flow simulations had indicated that\r\nthe vortex behavior is highly dependent on the local grid resolution both on body surface and space. The adjoint-based adaptation\r\nmethod used here is hoped to save grid points with a reasonable grid resolution for vortical flow simulations. The basic idea is\r\nto construct a new adaptive sensor in a grid adaptation process with the intent to tell where the elements should be smaller or\r\nlarger by introducing an adjoint formulation to relate the estimated functional error to local residual errors of both the primal and\r\nadjoint solutions.
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