國立虎尾科技大學 |

Advances in transitional flow modeling = applications to helicopter rotors /

紀錄類型:	書目-語言資料,印刷品 : Monograph/item
正題名/作者:	Advances in transitional flow modeling/ by Chunhua Sheng.
其他題名:	applications to helicopter rotors /
作者:	Sheng, Chunhua.
出版者:	Cham :Springer International Publishing : : 2017.,
面頁冊數:	xiii, 130 p. :ill., digital ; : 24 cm.;
Contained By:	Springer eBooks
標題:	Transition flow. -
電子資源:	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:

1164307
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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