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Advances in Transitional Flow Modeling

Applications to Helicopter Rotors

  • Chunhua Sheng
Book

Part of the SpringerBriefs in Applied Sciences and Technology book series (BRIEFSAPPLSCIENCES)

Table of contents

  1. Front Matter
    Pages i-xiii
  2. Chunhua Sheng
    Pages 1-7
  3. Chunhua Sheng
    Pages 9-19
  4. Chunhua Sheng
    Pages 21-54
  5. Chunhua Sheng
    Pages 55-82
  6. Chunhua Sheng
    Pages 83-130

About this book

Introduction

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.

Keywords

Computational Fluid Dynamics Turbulence Modelling Transition Modelling Rotorcraft Flow Separation Modelling and Simulation

Authors and affiliations

  • Chunhua Sheng
    • 1
  1. 1.University of ToledoToledoUSA

Bibliographic information

  • DOI https://doi.org/10.1007/978-3-319-32576-7
  • Copyright Information The Author(s) 2017
  • Publisher Name Springer, Cham
  • eBook Packages Engineering Engineering (R0)
  • Print ISBN 978-3-319-32575-0
  • Online ISBN 978-3-319-32576-7
  • Series Print ISSN 2191-530X
  • Series Online ISSN 2191-5318
  • Buy this book on publisher's site
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