Interactive airfoil calculations with higher-order viscous-flow equations
Author:
Affiliation:
1. University of Toronto Institute for Aerospace Studies, Toronto, Ontario, M3H 5T6 Canada
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/3.10701
Reference28 articles.
1. Multigrid acceleration of a relaxation procedure for the reduced Navier-Stokes equations
2. Higher-Order Boundary-Layer Theory
3. On the Calculation of Laminar and Turbulent Boundary Layers on Longitudinally Curved Surfaces
4. Numerical analysis of attached turbulent boundary layers along strongly curved surfaces
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2. Performance Analysis of Elliptic-Profile Airfoil Cascade for Designing Reversible Axial Flow Fans;AIAA Journal;2019-04
3. Computational study into the flow field developed around a cascade of NACA 0012 airfoils;Computer Methods in Applied Mechanics and Engineering;1998-12
4. Numerical simulation of the flow field around a cascade of NACA 0012 airfoils-effects of solidity and stagger;Computer Methods in Applied Mechanics and Engineering;1998-05
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