-
document
-
Souverein, L.J. (author)
Shock wave boundary layer interactions (SWBLI) are a common phenomenon in transonic and supersonic flows. The presence of shock waves, induced by specific geometrical configurations, causes a rapid increase of the pressure, which can lead to flow separation. Examples of such interactions are found in amongst others rocket engine nozzles and on...
doctoral thesis 2010
-
document
-
Humble, R.A. (author)
A fundamental experimental study is carried out to investigate the unsteady flow organization of an incident shock wave/turbulent boundary layer interaction at Mach 2.1. Planar and tomographic particle image velocimetry (PIV) are used in combination with data processing using the proper orthogonal decomposition (POD), complemented with hot-wire...
doctoral thesis 2009
Source URL (retrieved on 2024-05-10 12:03): https://repository.tudelft.nl/islandora/search/collection%253Air?collection=research&%3Bf%5B0%5D=mods_genre_s%3A%22doctoral%5C%20thesis%22&%3Bf%5B1%5D=mods_subject_topic_ss%3A%22microstructure%22&%3Bf%5B2%5D=RELS_EXT_isMemberOfCollection_uri_s%3A%22info%5C%3Afedora%5C/collection%5C%3Air%22&f%5B0%5D=mods_subject_topic_ss%3A%22turbulence%22&f%5B1%5D=mods_subject_topic_ss%3A%22interaction%22