Numerical Investigation on Aerodynamic Characteristics of Damaged Infinite Wings With Variation in Penetration Angle
Aerodynamic performance of a full span NACA 641-412 airfoil with a circular-shaped damage at various attack directions has been numerically investigated in this study. To assess the aerodynamic effects of different penetration angles in which threats such as projectiles can pass through the wings,...
| Main Authors: | , , |
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| Format: | Article |
| Language: | English |
| Published: |
Departamento de Ciência e Tecnologia Aeroespacial
2020-09-01
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| Series: | Journal of Aerospace Technology and Management |
| Subjects: | |
| Online Access: | https://www.scielo.br/pdf/jatm/v12/2175-9146-jatm-12-e4120.pdf |