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OverviewThis 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. Full Product DetailsAuthor: Nikolaus A. Adams , Wolfgang Schröder , Rolf Radespiel , Oskar J. HaidnPublisher: Springer Nature Switzerland AG Imprint: Springer Nature Switzerland AG Edition: 1st ed. 2021 Volume: 146 Weight: 0.658kg ISBN: 9783030538491ISBN 10: 3030538494 Pages: 419 Publication Date: 27 October 2021 Audience: Professional and scholarly , Professional & Vocational Format: Paperback Publisher's Status: Active Availability: Manufactured on demand  We will order this item for you from a manufactured on demand supplier. Table of ContentsCollaborative 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.- Effects 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.ReviewsAuthor InformationTab Content 6Author Website:Countries AvailableAll regions |
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