A Finite-Difference Method for Transonic Airfoil Design
β Scribed by Steger, Joseph L.; Klineberg, John M.
- Book ID
- 115497382
- Publisher
- American Institute of Aeronautics and Astronautics
- Year
- 1973
- Tongue
- English
- Weight
- 926 KB
- Volume
- 11
- Category
- Article
- ISSN
- 0001-1452
- DOI
- 10.2514/3.50502
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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
## Abstract A time marching integral equation method has been proposed here which does not have the limitation of the time linearized integral equation method in that the latter method can not satisfactorily simulate the shock wave motions. Firstly, a model problemβone dimensional initial and bound