Computation of transonic potential flow past wing-body configurations
β Scribed by S. K. Chakrabartty
- Book ID
- 112492872
- Publisher
- Springer Vienna
- Year
- 1990
- Tongue
- English
- Weight
- 515 KB
- Volume
- 81
- Category
- Article
- ISSN
- 0001-5970
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π SIMILAR VOLUMES
Using a finite-difference scheme, based on the relaxation method, the problem of constructing the flow field is solved for the noncirculation transonic flow of a nonviscous gas past three-dimensional objects. The calculation results are given for transonic gas flow past a triaxial ellipsoid when th
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