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Future Space-Transport-System Components under High Thermal and Mechanical Loads Results from the DFG Collaborative Research Center TRR40

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This 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 contro...

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Bibliographic Details
Other Authors: Adams, Nikolaus A. (Editor), Schröder, Wolfgang (Editor), Radespiel, Rolf (Editor), Haidn, Oskar J. (Editor), Sattelmayer, Thomas (Editor), Stemmer, Christian (Editor), Weigand, Bernhard (Editor)
Format: Electronic Book Chapter
Language:English
Published: Springer Nature 2021
Series:Notes on Numerical Fluid Mechanics and Multidisciplinary Design
Subjects:
Mechanics of fluids
Aerospace & aviation technology
Materials science
Engineering Fluid Dynamics
Aerospace Technology and Astronautics
Structural Materials
Rocket Propulsion
Multi-scale Modelling in Aerospace
Real-gas Thermodynamics
Multi-phase Flow Simulation
Compressible Shear-layer
Turbulent Heat Flux Model
LOX/CH4 Combustor
Multi-element Combustor Chamber
Wall Heat Transfer Prediction
SFB/TRR40
Open Access
Astronautics
Structural engineering
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Summary:This 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.
Physical Description:1 electronic resource (419 p.)
ISBN:978-3-030-53847-7
Access:Open Access

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