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Navier–Stokes computation of transonic vortices over a round leading edge delta wing

✍ Scribed by Bernhard Müller; Arthur Rizzi


Publisher
John Wiley and Sons
Year
1989
Tongue
English
Weight
1024 KB
Volume
9
Category
Article
ISSN
0271-2091

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An improved hybrid method for computing unsteady compressible viscous flows is presented. This method divides the computational domain into two zones. In the inner zone, the Navier -Stokes equations are solved using a diagonal form of an alternating-direction implicit (ADI) approximate factorisation