Three dimensional transonic visous flow computations are presented for a generic high-speed accelerator model which includes wing, body, fillets, and a no-flow through engine nacelle. Solutions are obtained from an algorithm for the compressible Navier-Stokes equations which incorporates an upwind-biased, flux-vector splitting approach along with longitudinally patched grids.
Transonic Navier-Stokes Solutions About a Complex High-Speed Accelerator Configuration
2004
22 pages
Report
No indication
English