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001 978-3-030-47461-4
003 DE-He213
005 20220801220026.0
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008 200730s2021 sz | s |||| 0|eng d
020 _a9783030474614
_9978-3-030-47461-4
024 7 _a10.1007/978-3-030-47461-4
_2doi
050 4 _aTA357-359
072 7 _aTGMF
_2bicssc
072 7 _aTEC009070
_2bisacsh
072 7 _aTGMF
_2thema
082 0 4 _a620.1064
_223
245 1 0 _aTransition Location Effect on Shock Wave Boundary Layer Interaction
_h[electronic resource] :
_bExperimental and Numerical Findings from the TFAST Project /
_cedited by Piotr Doerffer, Pawel Flaszynski, Jean-Paul Dussauge, Holger Babinsky, Patrick Grothe, Anna Petersen, Flavien Billard.
250 _a1st ed. 2021.
264 1 _aCham :
_bSpringer International Publishing :
_bImprint: Springer,
_c2021.
300 _aVIII, 540 p. 518 illus., 424 illus. in color.
_bonline resource.
336 _atext
_btxt
_2rdacontent
337 _acomputer
_bc
_2rdamedia
338 _aonline resource
_bcr
_2rdacarrier
347 _atext file
_bPDF
_2rda
490 1 _aNotes on Numerical Fluid Mechanics and Multidisciplinary Design,
_x1860-0824 ;
_v144
505 0 _aIntroduction – TFAST Overview -- WP-1 Reference Cases of Laminar and Turbulent Interactions -- WP-2 Basic Investigation of Transition Effect -- WP-3 Internal Flows – Compressors -- WP-4 Internal Flows – Turbine -- WP-5 External Flows – Wing -- Closing Remarks.
520 _aThis book presents experimental and numerical findings on reducing shock-induced separation by applying transition upstream the shock wave. The purpose is to find out how close to the shock wave the transition should be located in order to obtain favorable turbulent boundary layer interaction. The book shares findings obtained using advanced flow measurement methods and concerning e.g. the transition location, boundary layer characteristics, and the detection of shock wave configurations. It includes a number of experimental case studies and CFD simulations that offer valuable insights into the flow structure. It covers RANS/URANS methods for the experimental test section design, as well as more advanced techniques, such as LES, hybrid methods and DNS for studying the transition and shock wave interaction in detail. The experimental and numerical investigations presented here were conducted by sixteen different partners in the context of the TFAST Project. The general focus is on determining if and how it is possible to improve flow performance in comparison to laminar interaction. The book mainly addresses academics and professionals whose work involves the aerodynamics of internal and external flows, as well as experimentalists working with compressible flows. It will also be of benefit for CFD developers and users, and for students of aviation and propulsion systems alike.
650 0 _aFluid mechanics.
_92810
650 0 _aContinuum mechanics.
_93467
650 0 _aEngines.
_932152
650 0 _aThermodynamics.
_93554
650 0 _aHeat engineering.
_95144
650 0 _aHeat transfer.
_932329
650 0 _aMass transfer.
_94272
650 1 4 _aEngineering Fluid Dynamics.
_947901
650 2 4 _aContinuum Mechanics.
_93467
650 2 4 _aEngine Technology.
_932154
650 2 4 _aEngineering Thermodynamics, Heat and Mass Transfer.
_932330
700 1 _aDoerffer, Piotr.
_eeditor.
_4edt
_4http://id.loc.gov/vocabulary/relators/edt
_947902
700 1 _aFlaszynski, Pawel.
_eeditor.
_4edt
_4http://id.loc.gov/vocabulary/relators/edt
_947903
700 1 _aDussauge, Jean-Paul.
_eeditor.
_4edt
_4http://id.loc.gov/vocabulary/relators/edt
_947904
700 1 _aBabinsky, Holger.
_eeditor.
_4edt
_4http://id.loc.gov/vocabulary/relators/edt
_947905
700 1 _aGrothe, Patrick.
_eeditor.
_4edt
_4http://id.loc.gov/vocabulary/relators/edt
_947906
700 1 _aPetersen, Anna.
_eeditor.
_4edt
_4http://id.loc.gov/vocabulary/relators/edt
_947907
700 1 _aBillard, Flavien.
_eeditor.
_4edt
_4http://id.loc.gov/vocabulary/relators/edt
_947908
710 2 _aSpringerLink (Online service)
_947909
773 0 _tSpringer Nature eBook
776 0 8 _iPrinted edition:
_z9783030474607
776 0 8 _iPrinted edition:
_z9783030474621
776 0 8 _iPrinted edition:
_z9783030474638
830 0 _aNotes on Numerical Fluid Mechanics and Multidisciplinary Design,
_x1860-0824 ;
_v144
_947910
856 4 0 _uhttps://doi.org/10.1007/978-3-030-47461-4
912 _aZDB-2-ENG
912 _aZDB-2-SXE
942 _cEBK
999 _c78119
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