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Transitional flow past low Re aerofoil

IR@NAL: CSIR-National Aerospace Laboratories, Bangalore

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Field Value
 
Title Transitional flow past low Re aerofoil
 
Creator Subrahmanya, MB
Rajani, BN
Kulkarni, DS
Rajesh, A
 
Subject Fluid Mechanics and Thermodynamics
 
Description The Menter’s Gamma −Re_Theta SST model has been used to analyse the low Re aerofoil at Re = 114000. The capability of this model in predicting transition onset and Laminar Separation Bubble (LSB) has been demonstrated.
 
Date 2015
 
Type Conference or Workshop Item
PeerReviewed
 
Identifier Subrahmanya, MB and Rajani, BN and Kulkarni, DS and Rajesh, A (2015) Transitional flow past low Re aerofoil. In: 17th Annual CFD Symposium, CFD Division, AeSI, 11-08-2015, NAL, Bangalore.
 
Relation http://nal-ir.nal.res.in/12494/