The creation of lift by sharp-edged delta wings. An analysis of a self-adaptive numerical simulation using the concept of vorticity content

DOI10.1016/S0034-1223(98)80007-9zbMath0936.76055WikidataQ126556586 ScholiaQ126556586MaRDI QIDQ4246377

R. Hentschel

Publication date: 18 May 2000

Published in: Aerospace Science and Technology (Search for Journal in Brave)

zbMATH Keywords

transonic flowvortex layersdelta wing geometryEuler simulationsgeneration of circulationNavier-Stokes simulationsself-adaptive method AMRFLEX3D

Mathematics Subject Classification ID

Transonic flows (76H05) Finite difference methods applied to problems in fluid mechanics (76M20)

Uses Software

• AMRFLEX3D

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