Computational study into the flow field developed around a cascade of NACA 0012 airfoils
type: Item
instance of: scholarly article
title: Computational study into the flow field developed around a cascade of NACA 0012 airfoils
zbMATH Open document ID: 0951.76049
DOI: 10.1016/S0045-7825(98)00104-2
author: Yanyan Li
published in: Computer Methods in Applied Mechanics and Engineering
publication date: 2000-12-13T00:00:00Z
Mathematics Subject Classification ID: 76M12
Mathematics Subject Classification ID: 76G25
Mathematics Subject Classification ID: 76F40
Mathematics Subject Classification ID: 76F60
zbMATH DE Number: 1373282
zbMATH Keywords: \(k\)-epsilon model
zbMATH Keywords: separation point
zbMATH Keywords: boundary layer
zbMATH Keywords: cascade of NACA 0012 airfoils
zbMATH Keywords: control volume approach
zbMATH Keywords: two-dimensional incompressible Navier-Stokes equations
zbMATH Keywords: pressure contours
zbMATH Keywords: angles of attack
zbMATH Keywords: lift
zbMATH Keywords: drag
MaRDI profile type: Publication
cites work: Numerical study of the turbulent flow past an airfoil with trailing edge separation
description: scientific article; zbMATH DE number 1373282