Future space-transport-system components under high thermal and mechanical loads [electronic resource] : results from the DFG Collaborative Research Center TRR40 / Nikolaus A. Adams, Wolfgang Schröder, Rolf Radespiel, Oskar J. Haidn, Thomas Sattelmayer, Christian Stemmer, Bernhard Weigand, editors.
2021
TL783.4
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Title
Future space-transport-system components under high thermal and mechanical loads [electronic resource] : results from the DFG Collaborative Research Center TRR40 / Nikolaus A. Adams, Wolfgang Schröder, Rolf Radespiel, Oskar J. Haidn, Thomas Sattelmayer, Christian Stemmer, Bernhard Weigand, editors.
ISBN
9783030538477 (electronic bk.)
3030538478 (electronic bk.)
9783030538484 (print)
3030538486
9783030538491 (print)
3030538494
303053846X
9783030538460
3030538478 (electronic bk.)
9783030538484 (print)
3030538486
9783030538491 (print)
3030538494
303053846X
9783030538460
Published
Cham : Springer, 2021.
Language
English
Description
1 online resource.
Item Number
10.1007/978-3-030-53847-7 doi
Call Number
TL783.4
Dewey Decimal Classification
629.47/522
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.
Bibliography, etc. Note
Includes bibliographical references.
Access Note
Open access.
Digital File Characteristics
text file
PDF
Source of Description
Online resource; title from PDF title page (SpringerLink, viewed January 22, 2021).
Added Author
Series
Notes on numerical fluid mechanics and multidisciplinary design ; v. 146.
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Table of Contents
Collaborative 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
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