Typically, segregated methods have been used for the computation of incompressible ows whereas coupled solvers, for compressible ows. Compared to coupled solvers, segregated methods present the advantage of computational savings in RAM memory and CPU time, although at the cost of an inferior robustn
A panel method computation for oscillating aerofoil in compressible flow
β Scribed by Swee Hung Leong
- Publisher
- John Wiley and Sons
- Year
- 1990
- Tongue
- English
- Volume
- 29
- Category
- Article
- ISSN
- 0029-5981
No coin nor oath required. For personal study only.
π SIMILAR VOLUMES
A unified method for computing incompressible and compressible flows with Mach-uniform accuracy and efficiency is described. The method is equally applicable to stationary and nonstationary flows. A pressure-based discretisation on a staggered grid in general boundary-fitted coordinates is used for
A new numerical approach based on consistent operator splitting is presented for computing compressible, highly stratified flows in astrophysics. The algorithm is particularly designed to search for steady or almost steady solutions for the time-dependent Navier -Stokes equations, describing viscous