Advances in Transitional Flow Modeling : Applications to Helicopter Rotors.

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Bibliographic Details
Author / Creator:Sheng, Chunhua.
Imprint:Cham : Springer, [2017]
Description:1 online resource (140 pages)
Language:English
Series:SpringerBriefs in Applied Sciences and Technology
SpringerBriefs in applied sciences and technology.
Subject:
Format: E-Resource Book
URL for this record:http://pi.lib.uchicago.edu/1001/cat/bib/11269718
Hidden Bibliographic Details
Other authors / contributors:Wang, Jingyu.
ISBN:9783319325767
3319325760
3319325752
9783319325750
9783319325750
Digital file characteristics:text file PDF
Notes:Includes bibliographical references.
Print version record.
Summary: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.
Other form:Print version: Sheng, Chunhua. Advances in Transitional Flow Modeling : Applications to Helicopter Rotors. Cham : Springer International Publishing, ©2016 9783319325750
Standard no.:10.1007/978-3-319-32576-7

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505 0 |a Introduction -- Transition Prediction -- Transition Model -- Validations in 2-D Flows -- Applications for 3-D Rotors. 
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. 
504 |a Includes bibliographical references. 
650 0 |a Transition flow.  |0 http://id.loc.gov/authorities/subjects/sh85136945 
650 0 |a Rotors (Helicopters)  |0 http://id.loc.gov/authorities/subjects/sh85115510 
650 7 |a TECHNOLOGY & ENGINEERING  |x Engineering (General)  |2 bisacsh 
650 7 |a Rotors (Helicopters)  |2 fast  |0 (OCoLC)fst01100677 
650 7 |a Transition flow.  |2 fast  |0 (OCoLC)fst01154749 
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700 1 |a Wang, Jingyu. 
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