Comparative study of two dimensional boundary layer over NACA 23012 and NACA 23021 airfoils by using keller’s box method
This paper begins with general description on various methods for solving boundary layer equation. In particular, Prandtl's boundary layer equation is a simplified version of Navier-Stokes equation that is solved integrally. Order of magnitude analysis can be used to solve laminar and turbu...
| Asıl Yazarlar: | , , |
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| Materyal Türü: | Makale |
| Dil: | English |
| Baskı/Yayın Bilgisi: |
Penerbit UTHM
2022
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| Konular: | |
| Online Erişim: | http://eprints.uthm.edu.my/7709/1/J14547_893fab78e8617407a58a635075219a9d.pdf |