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Advances in transitional flow modeli...

Sheng, Chunhua.

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Advances in transitional flow modeling = applications to helicopter rotors /

Record Type:	Electronic resources : Monograph/item
Title/Author:	Advances in transitional flow modeling/ by Chunhua Sheng.
Reminder of title:	applications to helicopter rotors /
Author:	Sheng, Chunhua.
Published:	Cham :Springer International Publishing : : 2017.,
Description:	xiii, 130 p. :ill., digital ;24 cm.
[NT 15003449]:	Introduction -- Related Works -- Computational Fluid Dynamic Method -- Turbulence Modeling Method -- Validation of Transition Models -- Applications to Helicopter Rotors -- Recommendations.
Contained By:	Springer eBooks
Subject:	Transition flow. -
Online resource:	http://dx.doi.org/10.1007/978-3-319-32576-7
ISBN:	9783319325767

Advances in transitional flow modeling = applications to helicopter rotors /
Sheng, Chunhua.

Advances in transitional flow modelingapplications to helicopter rotors /[electronic resource] :by Chunhua Sheng. - Cham :Springer International Publishing :2017. - xiii, 130 p. :ill., digital ;24 cm. - SpringerBriefs in applied sciences and technology,2191-530X. - SpringerBriefs in applied sciences and technology..

Introduction -- Related Works -- Computational Fluid Dynamic Method -- Turbulence Modeling Method -- Validation of Transition Models -- Applications to Helicopter Rotors -- Recommendations.

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.

ISBN: 9783319325767

Standard No.: 10.1007/978-3-319-32576-7doiSubjects--Topical Terms:

2206885
Transition flow.

LC Class. No.: TA357.5.T87

Dewey Class. No.: 629.13232

Advances in transitional flow modeling = applications to helicopter rotors /
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100 1 $a Sheng, Chunhua. $3 3218352
245 1 0 $a Advances in transitional flow modeling $h [electronic resource] : $b applications to helicopter rotors / $c by Chunhua Sheng.
260 $a Cham : $b Springer International Publishing : $b Imprint: Springer, $c 2017.
300 $a xiii, 130 p. : $b ill., digital ; $c 24 cm.
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.
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650 0 $a Rotors (Helicopters) $3 2181191
650 1 4 $a Engineering. $3 586835
650 2 4 $a Aerospace Technology and Astronautics. $3 928116
650 2 4 $a Fluid- and Aerodynamics. $3 1066670
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