Experimental Investigation on Limit Cycle Wing Rock Effect on Wing Body Configuration Induced by Forebody Vortices
The purpose of this paper is to present the aerodynamic and flow characteristics of a slender body with a 30° swept wing configuration undergoing a limit cycle oscillation using a synchronous measurement and control technique of wing rock/particle image velocimetry/dynamic pressure associated w...
| Main Authors: | , , , |
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| Format: | Article |
| Language: | English |
| Published: |
Departamento de Ciência e Tecnologia Aeroespacial
2016-07-01
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| Series: | Journal of Aerospace Technology and Management |
| Subjects: | |
| Online Access: | http://www.jatm.com.br/ojs/index.php/jatm/article/view/627/541 |