Angle of Attack Effects on Boundary Layer Transition over a Flared Cone–Swept Fin Configuration
In our previous study, the transition behavior of a flared cone–swept fin configuration was investigated under an angle of attack (<i data-eusoft-scrollable-element="1">AoA</i>) of 0°. To further explore the role of <i data-eusoft-scrollable-element="1">AoA</i> in complex three-dimensional geometrie...
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| Egile Nagusiak: | , , , , , |
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| Formatua: | Artigo |
| Hizkuntza: | Inglês |
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MDPI AG
2025-09-01
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| Saila: | Aerospace |
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| Sarrera elektronikoa: | https://www.mdpi.com/2226-4310/12/9/824 |
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