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Interactive boundary-layer method for unsteady airfoil flows - Quasisteady model

✍ Scribed by CEBECI, TUNCER; JANG, HONG-MING

Book ID
120367919
Publisher
American Institute of Aeronautics and Astronautics
Year
1990
Tongue
English
Weight
723 KB
Volume
27
Category
Article
ISSN
0021-8669

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πŸ“œ SIMILAR VOLUMES

A hybrid boundary element β€” finite volum
A hybrid boundary element β€” finite volume method for unsteady transonic airfoil flows
✍ Hong Hu; Osama A. Kandil πŸ“‚ Article πŸ“… 1994 πŸ› Elsevier Science 🌐 English βš– 590 KB

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