Skin Friction Measurement on a Swept NACA 0015 Wing Using Oil Film Interferometry
AIAA AVIATION FORUM AND ASCEND 2024
2024-01-01
Conference paper
Electronic Resource
English
Active Flow Separation Control on a NACA 0015 Wing Using Fluidic Actuators (AIAA 2014-2364)
British Library Conference Proceedings | 2014
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