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001 978-3-319-32576-7
003 DE-He213
005 20220801221946.0
007 cr nn 008mamaa
008 161128s2017 sz | s |||| 0|eng d
020 _a9783319325767
_9978-3-319-32576-7
024 7 _a10.1007/978-3-319-32576-7
_2doi
050 4 _aTL1-4050
072 7 _aTRP
_2bicssc
072 7 _aTTDS
_2bicssc
072 7 _aTEC002000
_2bisacsh
072 7 _aTRP
_2thema
072 7 _aTTDS
_2thema
082 0 4 _a629.1
_223
100 1 _aSheng, Chunhua.
_eauthor.
_4aut
_4http://id.loc.gov/vocabulary/relators/aut
_958942
245 1 0 _aAdvances in Transitional Flow Modeling
_h[electronic resource] :
_bApplications to Helicopter Rotors /
_cby Chunhua Sheng.
250 _a1st ed. 2017.
264 1 _aCham :
_bSpringer International Publishing :
_bImprint: Springer,
_c2017.
300 _aXIII, 130 p. 114 illus., 101 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 _aSpringerBriefs in Applied Sciences and Technology,
_x2191-5318
505 0 _aIntroduction -- Related Works -- Computational Fluid Dynamic Method -- Turbulence Modeling Method -- Validation of Transition Models -- Applications to Helicopter Rotors -- Recommendations.
520 _aThis book provides a comprehensive description of numerical methods and validation processes for predicting transitional flows based on the Langtry–Menter local correlation-based transition model, integrated with both one-equation Spalart–Allmaras (S–A) and two-equation Shear Stress Transport (SST) turbulence models. A comparative study is presented to combine the respective merits of the two coupling methods in the context of predicting the boundary-layer transition phenomenon from fundamental benchmark flows to realistic helicopter rotors. The book will of interest to industrial practitioners working in aerodynamic design and the analysis of fixed-wing or rotary wing aircraft, while also offering advanced reading material for graduate students in the research areas of Computational Fluid Dynamics (CFD), turbulence modeling and related fields.
650 0 _aAerospace engineering.
_96033
650 0 _aAstronautics.
_958943
650 0 _aContinuum mechanics.
_93467
650 0 _aFluid mechanics.
_92810
650 1 4 _aAerospace Technology and Astronautics.
_958944
650 2 4 _aContinuum Mechanics.
_93467
650 2 4 _aEngineering Fluid Dynamics.
_958945
710 2 _aSpringerLink (Online service)
_958946
773 0 _tSpringer Nature eBook
776 0 8 _iPrinted edition:
_z9783319325750
776 0 8 _iPrinted edition:
_z9783319325774
830 0 _aSpringerBriefs in Applied Sciences and Technology,
_x2191-5318
_958947
856 4 0 _uhttps://doi.org/10.1007/978-3-319-32576-7
912 _aZDB-2-ENG
912 _aZDB-2-SXE
942 _cEBK
999 _c80245
_d80245