Einfluss des Dralls auf den Überschallnachlauf eines längsangeströmten zylindrischen Körpers

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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Bibliographic Details
Main Author: Weidner, Stephan (auth)
Format: eBook
Published: Karlsruhe KIT Scientific Publishing 2021
Subjects:
Online Access:Get fulltext
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005 20210212
020 |a KSP/1000118606 
024 7 |a 10.5445/KSP/1000118606  |c doi 
041 0 |h German 
042 |a dc 
100 1 |a Weidner, Stephan  |e auth 
245 1 0 |a Einfluss des Dralls auf den Überschallnachlauf eines längsangeströmten zylindrischen Körpers 
260 |a Karlsruhe  |b KIT Scientific Publishing  |c 2021 
300 |a 1 electronic resource (218 p.) 
856 |z Get fulltext  |u https://library.oapen.org/handle/20.500.12657/46722 
506 0 |a Open Access  |2 star  |f Unrestricted online access 
520 |a 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. 
540 |a Creative Commons 
546 |a German 
650 7 |a Mechanical engineering & materials  |2 bicssc 
653 |a Überschallnachlauf 
653 |a Drall 
653 |a Wirbelaufplatzen 
653 |a Windkanalmessungen 
653 |a Numerische Simulationen 
653 |a supersonic wake flow 
653 |a swirl 
653 |a vortex breakdown 
653 |a wind-tunnel measurements 
653 |a numerical simulations