Advances in Transitional Flow Modeling Applications to Helicopter Rotors
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Sprache:Englisch
Fr. 73.90
inkl. gesetzl. MwSt.,
Beschreibung
Produktdetails
Einband
Taschenbuch
Erscheinungsdatum
21.12.2016
Abbildungen
XIII, 114 illus., 101 illus. in color. With online files/update., farbige Illustrationen, schwarz-weiss Illustrationen
Verlag
SpringerSeitenzahl
130
Maße (L/B/H)
23.3/15.6/1.2 cm
Gewicht
230 g
Auflage
1st ed. 2017
Sprache
Englisch
ISBN
978-3-319-32575-0
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.
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