Advances in Transitional Flow Modeling Applications to Helicopter Rotors /

This 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)...

Πλήρης περιγραφή

Λεπτομέρειες βιβλιογραφικής εγγραφής
Κύριος συγγραφέας: Sheng, Chunhua (Συγγραφέας)
Συγγραφή απο Οργανισμό/Αρχή: SpringerLink (Online service)
Μορφή: Ηλεκτρονική πηγή Ηλ. βιβλίο
Γλώσσα:English
Έκδοση: Cham : Springer International Publishing : Imprint: Springer, 2017.
Σειρά:SpringerBriefs in Applied Sciences and Technology,
Θέματα:
Διαθέσιμο Online:Full Text via HEAL-Link
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020 |a 9783319325767  |9 978-3-319-32576-7 
024 7 |a 10.1007/978-3-319-32576-7  |2 doi 
040 |d GrThAP 
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072 7 |a TEC002000  |2 bisacsh 
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100 1 |a Sheng, Chunhua.  |e author. 
245 1 0 |a Advances in Transitional Flow Modeling  |h [electronic resource] :  |b Applications to Helicopter Rotors /  |c by Chunhua Sheng. 
264 1 |a Cham :  |b Springer International Publishing :  |b Imprint: Springer,  |c 2017. 
300 |a XIII, 130 p. 114 illus., 101 illus. in color.  |b online resource. 
336 |a text  |b txt  |2 rdacontent 
337 |a computer  |b c  |2 rdamedia 
338 |a online resource  |b cr  |2 rdacarrier 
347 |a text file  |b PDF  |2 rda 
490 1 |a SpringerBriefs in Applied Sciences and Technology,  |x 2191-530X 
505 0 |a Introduction -- Related Works -- Computational Fluid Dynamic Method -- Turbulence Modeling Method -- Validation of Transition Models -- Applications to Helicopter Rotors -- Recommendations. 
520 |a This 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 |a Engineering. 
650 0 |a Fluids. 
650 0 |a Fluid mechanics. 
650 0 |a Aerospace engineering. 
650 0 |a Astronautics. 
650 1 4 |a Engineering. 
650 2 4 |a Aerospace Technology and Astronautics. 
650 2 4 |a Fluid- and Aerodynamics. 
650 2 4 |a Engineering Fluid Dynamics. 
710 2 |a SpringerLink (Online service) 
773 0 |t Springer eBooks 
776 0 8 |i Printed edition:  |z 9783319325750 
830 0 |a SpringerBriefs in Applied Sciences and Technology,  |x 2191-530X 
856 4 0 |u http://dx.doi.org/10.1007/978-3-319-32576-7  |z Full Text via HEAL-Link 
912 |a ZDB-2-ENG 
950 |a Engineering (Springer-11647)