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135   $aurmn|---annan
181   $ctxt$2rdacontent
182   $cc$2rdamedia
183   $acr$2rdacarrier
200 00$aEinfluss des Dralls auf den U?berschallnachlauf eines la?ngsangestro?mten zylindrischen Ko?rpers
210   $aKarlsruhe$cKIT Scientific Publishing$d2021
215   $a1 online resource (218 p.)
225 1 $aSchriftenreihe des Instituts fur Stromungsmechanik, Karlsruher Institut fur Technologie
311 08$a3-7315-1030-8 
330   $aThis 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.
606   $aMechanical engineering & materials$2bicssc
610   $aDrall
610   $anumerical simulations
610   $aNumerische Simulationen
610   $asupersonic wake flow
610   $aswirl
610   $aU?berschallnachlauf
610   $avortex breakdown
610   $awind-tunnel measurements
610   $aWindkanalmessungen
610   $aWirbelaufplatzen
615  7$aMechanical engineering & materials
906   $aBOOK
912   $a9910805667203321
996   $aEinfluss des Dralls auf den Überschallnachlauf eines längsangeströmten zylindrischen Körpers$93908042
997   $aUNINA