Sheng, Chunhua. <br/><br/>
Advances in Transitional Flow Modeling  Applications to Helicopter Rotors /  [electronic resource] : 
by Chunhua Sheng. 
 - 1st ed. 2017. 
 - XIII, 130 p. 114 illus., 101 illus. in color.  online resource. 
 - SpringerBriefs in Applied Sciences and Technology,  2191-5318 .
 - SpringerBriefs in Applied Sciences and Technology, .
<br/><br/>Introduction -- Related Works -- Computational Fluid Dynamic Method -- Turbulence Modeling Method -- Validation of Transition Models -- Applications to Helicopter Rotors -- Recommendations. 
<br/><br/> 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. 
<br/><br/><label>ISBN: </label>9783319325767 
<br/><br/><label>Standard No.: </label>10.1007/978-3-319-32576-7  doi 
<br/><br/><label>Subjects--Topical Terms: </label><br/>Aerospace engineering.<br/>Astronautics.<br/>Continuum mechanics.<br/>Fluid mechanics.<br/>Aerospace Technology and Astronautics.<br/>Continuum Mechanics.<br/>Engineering Fluid Dynamics.
<br/><br/><label>LC Class. No.: </label>TL1-4050 
<br/><br/><label>Dewey Class. No.: </label>629.1