NASA NTRS · 19870010809
Simulation of transonic viscous wing and wing-fuselage flows using zonal methods
Abstract
The thin-layer Navier-Stokes equations are coupled with a zonal scheme (or domain-decomposition method) to develop the Transonic Navier-Stokes (TNS) wing-alone code. The TNS has a total of 4 zones and is extended to a total of 16 zones for the wing-fuselage version of the code. Results are compared on the Cray X-MP-48 and compared with experimental data.
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Flores, Jolen. 1987-03-01. Simulation of transonic viscous wing and wing-fuselage flows using zonal methods. https://ntrs.nasa.gov/citations/19870010809
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