978-3-7315-1030-7.pdf

This study investigates the effects of swirl on the supersonic wake of longitudinally-aligned axisymmetric afterbodies. The swirl was introduced upstream of the base corner by either spinning non-canted or non-spinning canted fins. Depending on the introduced swirl rate, both the experimental and nu...

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Έκδοση: KIT Scientific Publishing 2021
id oapen-20.500.12657-46722
record_format dspace
spelling oapen-20.500.12657-467222021-02-16T02:17:19Z Einfluss des Dralls auf den Überschallnachlauf eines längsangeströmten zylindrischen Körpers Weidner, Stephan Überschallnachlauf Drall Wirbelaufplatzen Windkanalmessungen Numerische Simulationen supersonic wake flow swirl vortex breakdown wind-tunnel measurements numerical simulations bic Book Industry Communication::T Technology, engineering, agriculture::TG Mechanical engineering & materials This study investigates the effects of swirl on the supersonic wake of longitudinally-aligned axisymmetric afterbodies. The swirl was introduced upstream of the base corner by either spinning non-canted or non-spinning canted fins. Depending on the introduced swirl rate, both the experimental and numerical results show two distinctively different wake flow structures. The fluid-dynamic processes present in the rotating wakes and the resulting structural changes are analyzed in detail. 2021-02-12T11:44:13Z 2021-02-12T11:44:13Z 2021 book ONIX_20210212_9783731510307_9 https://library.oapen.org/handle/20.500.12657/46722 ger Schriftenreihe des Instituts fur Stromungsmechanik, Karlsruher Institut fur Technologie application/pdf Attribution-ShareAlike 4.0 International 978-3-7315-1030-7.pdf KIT Scientific Publishing 10.5445/KSP/1000118606 This study investigates the effects of swirl on the supersonic wake of longitudinally-aligned axisymmetric afterbodies. The swirl was introduced upstream of the base corner by either spinning non-canted or non-spinning canted fins. Depending on the introduced swirl rate, both the experimental and numerical results show two distinctively different wake flow structures. The fluid-dynamic processes present in the rotating wakes and the resulting structural changes are analyzed in detail. 10.5445/KSP/1000118606 44e29711-8d53-496b-85cc-3d10c9469be9 7 218 Karlsruhe open access
institution OAPEN
collection DSpace
language ger
description This study investigates the effects of swirl on the supersonic wake of longitudinally-aligned axisymmetric afterbodies. The swirl was introduced upstream of the base corner by either spinning non-canted or non-spinning canted fins. Depending on the introduced swirl rate, both the experimental and numerical results show two distinctively different wake flow structures. The fluid-dynamic processes present in the rotating wakes and the resulting structural changes are analyzed in detail.
title 978-3-7315-1030-7.pdf
spellingShingle 978-3-7315-1030-7.pdf
title_short 978-3-7315-1030-7.pdf
title_full 978-3-7315-1030-7.pdf
title_fullStr 978-3-7315-1030-7.pdf
title_full_unstemmed 978-3-7315-1030-7.pdf
title_sort 978-3-7315-1030-7.pdf
publisher KIT Scientific Publishing
publishDate 2021
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