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001430875 001__ 1430875
001430875 003__ OCoLC
001430875 005__ 20230308003210.0
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001430875 008__ 201103s2021\\\\sz\\\\\\ob\\\\000\0\eng\d
001430875 019__ $$a1225933394$$a1240522838$$a1241066536$$a1249248596
001430875 020__ $$a9783030538477$$q(electronic bk.)
001430875 020__ $$a3030538478$$q(electronic bk.)
001430875 020__ $$a9783030538484$$q(print)
001430875 020__ $$a3030538486
001430875 020__ $$a9783030538491$$q(print)
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001430875 0247_ $$a10.1007/978-3-030-53847-7$$2doi
001430875 035__ $$aSP(OCoLC)1202759472
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001430875 049__ $$aISEA
001430875 050_4 $$aTL783.4
001430875 08204 $$a629.47/522$$223
001430875 24500 $$aFuture space-transport-system components under high thermal and mechanical loads :$$bresults from the DFG Collaborative Research Center TRR40 /$$cNikolaus A. Adams, Wolfgang Schröder, Rolf Radespiel, Oskar J. Haidn, Thomas Sattelmayer, Christian Stemmer, Bernhard Weigand, editors.
001430875 260__ $$aCham :$$bSpringer,$$c2021.
001430875 300__ $$a1 online resource
001430875 336__ $$atext$$btxt$$2rdacontent
001430875 337__ $$acomputer$$bc$$2rdamedia
001430875 338__ $$aonline resource$$bcr$$2rdacarrier
001430875 347__ $$atext file$$2rdaft$$0http://rdaregistry.info/termList/fileType/1002
001430875 347__ $$bPDF
001430875 4901_ $$aNotes on Numerical Fluid Mechanics and Multidisciplinary Design,$$x1612-2909 ;$$v146
001430875 504__ $$aIncludes bibliographical references.
001430875 5050_ $$aCollaborative Research for Future Space Transportation Systems -- Innovative Cooling for Rocket Combustion Chambers -- Film Cooling in Rocket Nozzle -- Heat Transfer in Pulsating Flow and its Impact on Temperature Distribution and Damping Performance of Acoustic Resonators -- E
001430875 5060_ $$aOpen access.$$5GW5XE
001430875 520__ $$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.
001430875 588__ $$aOnline resource; title from PDF title page (SpringerLink, viewed January 22, 2021).
001430875 650_0 $$aLiquid propellant rockets$$xFuel tanks$$xThermodynamics.
001430875 650_0 $$aLiquid propellant rocket engines.
001430875 655_0 $$aElectronic books.
001430875 7001_ $$aAdams, N.$$q(Nikolaus),$$eeditor.
001430875 7001_ $$aSchröder, Wolfgang,$$cDipl.-Ing.,$$eeditor.
001430875 7001_ $$aRadespiel, Rolf,$$eeditor.
001430875 7001_ $$aHaidn, Oskar J.,$$eeditor.
001430875 7001_ $$aSattelmayer, Thomas,$$eeditor.
001430875 7001_ $$aStemmer, Christian,$$eeditor.
001430875 7001_ $$aWeigand, Bernhard,$$d1962-$$eeditor.
001430875 77608 $$iPrint version:$$tFuture space-transport-system components under high thermal and mechanical loads.$$dCham : Springer, 2021$$z303053846X$$z9783030538460$$w(OCoLC)1159045772
001430875 830_0 $$aNotes on numerical fluid mechanics and multidisciplinary design ;$$vv. 146.$$x1612-2909
001430875 852__ $$bebk
001430875 85640 $$3Springer Nature$$uhttps://link.springer.com/10.1007/978-3-030-53847-7$$zOnline Access$$91397441.2
001430875 909CO $$ooai:library.usi.edu:1430875$$pGLOBAL_SET
001430875 980__ $$aBIB
001430875 980__ $$aEBOOK
001430875 982__ $$aEbook
001430875 983__ $$aOnline
001430875 994__ $$a92$$bISE