2010•Aeronautical Computing TechniqueRequires access

Applications of Multi-grid Scheme in the Hypersonic Inlet

Yin Feng-e

Abstract

With the development of computer technology and fluid dynamics,multi-grid scheme has been widely used in solving Euler equations and Navier-Stokes equations.In this thesis,I research the possibility of using the method to optimize the numerical simulation of hypersonic inlet.Some practical examples of simulation results show that the method has good validity and potential to practical application.

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Available abstract

Key concepts: Hypersonic speed, Scheme (mathematics), Grid, Euler equations, Inlet, Aerospace engineering, Euler's formula, Computer science