Unsteady transonic wing flow computations using field-boundary element methods
β Scribed by Hong Hu
- Publisher
- Elsevier Science
- Year
- 1992
- Tongue
- English
- Weight
- 539 KB
- Volume
- 10
- Category
- Article
- ISSN
- 0955-7997
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π SIMILAR VOLUMES
A hybrid boundary element -finite volume method for unsteady transonic flow computation has been developed. In this method, the unsteady Euler equations in a moving frame of reference are solved in a small embedded domain (inner domain) around the airfoil using an implicit finite volume scheme. The
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