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document
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Serpieri, J. (author), Kotsonis, M. (author)
In this work the flow visualization of the transition pattern occurring on a swept wing in a subsonic flow is presented. This is done by means of fluorescent oil flow technique and boundary layer hot-wire scans. The experiment was performed at Reynolds number of 2:15 . 106 and at angle of attack of -3ยบ. At these conditions, three different flows...
conference paper 2015
Source URL (retrieved on 2024-04-23 17:52): https://repository.tudelft.nl/islandora/search/author%3A%22Kotsonis%2C%20M.%22?collection=research&%3Bamp%3Bf%5B0%5D=mods_name_personal_author_namePart_family_ss%3A%22Serpieri%22&%3Bamp%3Bf%5B1%5D=mods_subject_topic_ss%3A%22Boundary%5C%20layer%5C%20stability%22&%3Bamp%3Bsort=mods_genre_s%20asc&%3Bf%5B0%5D=mods_subject_topic_ss%3A%22Synthetic%5C%20jet%22&f%5B0%5D=mods_subject_topic_ss%3A%223D%5C%20subsonic%5C%20boundary%5C%20layer%5C%20transition%22