New insights from high-resolution compressible DNS studies on an LPT blade boundary layer-Reference-Cited by-同舟云学术

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New insights from high-resolution compressible DNS studies on an LPT blade boundary layer

Published:2017-08 Issue: Volume:153 Page:49-60
ISSN:0045-7930
Container-title:Computers & Fluids
language:en
Short-container-title:Computers & Fluids

Author:

Ranjan Rajesh,Deshpande S.M.,Narasimha Roddam

Publisher

Elsevier BV

Subject

General Engineering,General Computer Science

Reference36 articles.

1. Direct numerical simulations of a two-dimensional viscous flow in a shocktube using a kinetic energy preserving scheme;Allaneau;AIAA paper,2009

2. Direct numerical simulations of plunging airfoils;Allaneau,2010

3. Computational fluid dynamics: principles and applications:(book with accompanying CD);Blazek,2005

4. Development of blade profiles for low-pressure turbine applications;Curtis;J Turbomach,1997

5. Case 3.3: Taylor-Green vortex evolution;Diosady,2015

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2. Numerical prediction of largely separated flows in low-pressure turbine blades with high loading;Sādhanā;2024-02-10

3. Loss reduction in the compressor corner region via blade cooling;International Journal of Mechanical Sciences;2024-01

4. A Critical Comparison of DNS Versus RANS Model Results on an HPT Blade for a Small Engine;Journal of Aerospace Sciences and Technologies;2023-07-29

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