LEADER 04289nam 22007575 450 001 9910424948303321 005 20251113162001.0 010 $a978-3-030-53847-7$b(electronic book) 010 $a3-030-53847-8 024 7 $a10.1007/978-3-030-53847-7 035 $a(OCoLC)1202759472 035 $a(DE-He213)978-3-030-53847-7 035 $a(MiAaPQ)EBC6381145 035 $a(Au-PeEL)EBL6381145 035 $a(OCoLC)1243554957 035 $a(oapen)https://directory.doabooks.org/handle/20.500.12854/35998 035 $a(PPN)258059915 035 $a(CKB)4100000011528387 035 $a(ODN)ODN0010068978 035 $a(oapen)doab35998 035 $a(EXLCZ)994100000011528387 100 $a20201026d2021 u| 0 101 0 $aeng 135 $aurnnu|||uuuuu 181 $ctxt$2rdacontent 182 $cc$2rdamedia 183 $acr$2rdacarrier 200 10$aFuture Space-Transport-System Components under High Thermal and Mechanical Loads $eResults from the DFG Collaborative Research Center TRR40 /$fedited by Nikolaus A. Adams, Wolfgang Schröder, Rolf Radespiel, Oskar J. Haidn, Thomas Sattelmayer, Christian Stemmer, Bernhard Weigand 205 $a1st ed. 2021. 210 1$aCham :$cSpringer International Publishing :$cImprint: Springer,$d2021. 215 $a1 online resource (ix, 419 pages 273) $cillustrations in color 225 1 $aNotes on Numerical Fluid Mechanics and Multidisciplinary Design,$x1860-0824 ;$v146 311 0 $a3-030-53846-X 327 $aCollaborative Research for Future Space Transportation Systems -- Innovative Cooling for Rocket Combustion Chambers -- Film Cooling in Rocket Nozzle -- Heat Transfer in Pulsating Flow and its Impact on Temperature Distribution and Damping Performance of Acoustic Resonators -- E?ects of a Launcher?s External Fow on a Dual-Bell Nozzle Flow -- Interaction of Wake and Propulsive Jet Flow of a Generic Space Launcher -- Numerical Analysis of the Turbulent Wake for a Generic Space Launcher with a Dual-Bell Nozzle. 330 $aThis open access book presents the findings of Collaborative Research Center Transregio 40 (TRR40), initiated in July 2008 and funded by the German Research Foundation (DFG). Gathering innovative design concepts for thrust chambers and nozzles, as well as cutting-edge methods of aft-body flow control and propulsion-component cooling, it brings together fundamental research undertaken at universities, testing carried out at the German Aerospace Center (DLR) and industrial developments from the ArianeGroup. With a particular focus on heat transfer analyses and novel cooling concepts for thermally highly loaded structures, the book highlights the aft-body flow of the space transportation system and its interaction with the nozzle flow, which are especially critical during the early phase of atmospheric ascent. Moreover, it describes virtual demonstrators for combustion chambers and nozzles, and discusses their industrial applicability. As such, it is a timely resource for researchers, graduate students and practitioners. . 410 0$aNotes on Numerical Fluid Mechanics and Multidisciplinary Design,$x1860-0824 ;$v146 606 $aFluid mechanics 606 $aAerospace engineering 606 $aAstronautics 606 $aBuilding materials 606 $aEngineering Fluid Dynamics 606 $aAerospace Technology and Astronautics 606 $aStructural Materials 615 0$aFluid mechanics. 615 0$aAerospace engineering. 615 0$aAstronautics. 615 0$aBuilding materials. 615 14$aEngineering Fluid Dynamics. 615 24$aAerospace Technology and Astronautics. 615 24$aStructural Materials. 676 $a620.1064 686 $aTEC002000$aTEC009070$aTEC021000$2bisacsh 700 $aAdams$b Nikolaus A$01830640 702 $aAdams$b Nikolaus A. 702 $aSchröder$b Wolfgang 702 $aRadespiel$b Rolf 702 $aHaidn$b Oskar J. 702 $aSattelmayer$b Thomas 702 $aStemmer$b Christian 702 $aWeigand$b Bernhard 801 0$bMiAaPQ 801 1$bMiAaPQ 801 2$bOD$ 912 $a9910424948303321 996 $aFuture Space-Transport-System Components under High Thermal and Mechanical Loads$94401126 997 $aUNINA