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)...

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Bibliographic Details
Main Author: Sheng, Chunhua.
Other Authors: Wang, Jingyu.
Format: eBook
Language: English
Published: Cham : Springer, [2017]
Series: SpringerBriefs in applied sciences and technology.
Subjects:
tekutiny
mechanika tekutin
letecké inženýrství
počítačová mechanika tekutin
fluids
fluid mechanics
aircraft engineering
computational fluid dynamics
elektronické knihy
monografie
electronic books
monographs
ISBN: 9783319325767
9783319325750
Physical Description: 1 online resource (140 pages)

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Table of contents

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072 7 |a 532  |x Mechanika tekutin obecně. Mechanika kapalin  |2 Konspekt  |9 6 
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080 |a 532:004.94  |2 MRF 
080 |a (0.034.2:08)   |2 MRF 
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100 1 |a Sheng, Chunhua. 
245 1 0 |a Advances in Transitional Flow Modeling :  |b Applications to Helicopter Rotors. 
260 |a Cham :  |b Springer,  |c [2017] 
300 |a 1 online resource (140 pages) 
336 |a text  |b txt  |2 rdacontent 
337 |a počítač  |b c  |2 rdamedia 
338 |a online zdroj  |b cr  |2 rdacarrier 
490 1 |a SpringerBriefs in Applied Sciences and Technology 
504 |a Includes bibliographical references. 
506 |a Plný text je dostupný pouze z IP adres počítačů Univerzity Tomáše Bati ve Zlíně nebo vzdáleným přístupem pro zaměstnance a studenty 
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.- Resumé vydavatel 
590 |a SpringerLink  |b Springer Complete eBooks 
650 0 7 |a tekutiny  |2 czenas  |7 ph126494 
650 0 7 |a mechanika tekutin  |2 czenas  |7 ph115249 
650 0 7 |a letecké inženýrství  |2 czenas  |7 ph920311 
650 0 7 |a počítačová mechanika tekutin  |2 czenas  |7 ph507303 
650 0 9 |a fluids  |2 eczenas 
650 0 9 |a fluid mechanics  |2 eczenas 
650 0 9 |a aircraft engineering  |2 eczenas 
650 0 9 |a computational fluid dynamics  |2 eczenas 
655 7 |a elektronické knihy  |7 fd186907  |2 czenas 
655 7 |a monografie  |7 fd132842   |2 czenas 
655 9 |a electronic books  |2 eczenas 
655 9 |a monographs  |2 eczenas 
700 1 |a Wang, Jingyu. 
776 0 8 |i Print version:  |a Sheng, Chunhua.  |t Advances in Transitional Flow Modeling : Applications to Helicopter Rotors.  |d Cham : Springer International Publishing, ©2016  |z 9783319325750 
830 0 |a SpringerBriefs in applied sciences and technology. 
856 4 0 |u https://proxy.k.utb.cz/login?url=https://link.springer.com/10.1007/978-3-319-32576-7  |y Plný text 
942 |2 udc 
992 |c NTK-SpringerENG 
993 |x NEPOSILAT  |y EIZ 

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