Advances in Transitional Flow Modeling (Record no. 80245)

000 -LEADER
fixed length control field 03090nam a22005655i 4500
001 - CONTROL NUMBER
control field 978-3-319-32576-7
005 - DATE AND TIME OF LATEST TRANSACTION
control field 20220801221946.0
008 - FIXED-LENGTH DATA ELEMENTS--GENERAL INFORMATION
fixed length control field 161128s2017 sz | s |||| 0|eng d
020 ## - INTERNATIONAL STANDARD BOOK NUMBER
ISBN 9783319325767
-- 978-3-319-32576-7
082 04 - CLASSIFICATION NUMBER
Call Number 629.1
100 1# - AUTHOR NAME
Author Sheng, Chunhua.
245 10 - TITLE STATEMENT
Title Advances in Transitional Flow Modeling
Sub Title Applications to Helicopter Rotors /
250 ## - EDITION STATEMENT
Edition statement 1st ed. 2017.
300 ## - PHYSICAL DESCRIPTION
Number of Pages XIII, 130 p. 114 illus., 101 illus. in color.
490 1# - SERIES STATEMENT
Series statement SpringerBriefs in Applied Sciences and Technology,
505 0# - FORMATTED CONTENTS NOTE
Remark 2 Introduction -- Related Works -- Computational Fluid Dynamic Method -- Turbulence Modeling Method -- Validation of Transition Models -- Applications to Helicopter Rotors -- Recommendations.
520 ## - SUMMARY, ETC.
Summary, etc 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.
856 40 - ELECTRONIC LOCATION AND ACCESS
Uniform Resource Identifier https://doi.org/10.1007/978-3-319-32576-7
942 ## - ADDED ENTRY ELEMENTS (KOHA)
Koha item type eBooks
264 #1 -
-- Cham :
-- Springer International Publishing :
-- Imprint: Springer,
-- 2017.
336 ## -
-- text
-- txt
-- rdacontent
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-- computer
-- c
-- rdamedia
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-- online resource
-- cr
-- rdacarrier
347 ## -
-- text file
-- PDF
-- rda
650 #0 - SUBJECT ADDED ENTRY--SUBJECT 1
-- Aerospace engineering.
650 #0 - SUBJECT ADDED ENTRY--SUBJECT 1
-- Astronautics.
650 #0 - SUBJECT ADDED ENTRY--SUBJECT 1
-- Continuum mechanics.
650 #0 - SUBJECT ADDED ENTRY--SUBJECT 1
-- Fluid mechanics.
650 14 - SUBJECT ADDED ENTRY--SUBJECT 1
-- Aerospace Technology and Astronautics.
650 24 - SUBJECT ADDED ENTRY--SUBJECT 1
-- Continuum Mechanics.
650 24 - SUBJECT ADDED ENTRY--SUBJECT 1
-- Engineering Fluid Dynamics.
830 #0 - SERIES ADDED ENTRY--UNIFORM TITLE
-- 2191-5318
912 ## -
-- ZDB-2-ENG
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-- ZDB-2-SXE

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