Performance of an airfoil at low reynolds number

Premalatha, and Ramamoorthy, P (1991) Performance of an airfoil at low reynolds number. Technical Report. National Aeronautical Laboratory, Bangalore, India.

[img] PDF
tr_pd_cf_9102_R74769.pdf
Restricted to Repository staff only

Download (2MB)

Abstract

A new airfoil performance software is developed by combining two independent codes . The first one is based on Theodorsen's thick airfoil theory and second one is a boundary layer code based on the integral method.13; The lift and pitching moment coefficients are obtained by Theodorsen's theory suitably modified for the viscous effects.The comparison between this code and NCSU code 'and experiments for a few low drag airfoil show good correlation and hence the code has great potential for further development.

Item Type: Monograph (Technical Report)
Uncontrolled Keywords: Airfoil;Performance
Subjects: AERONAUTICS > Aeronautics (General)
Depositing User: Users 20 not found.
Date Deposited: 24 Jun 2006
Last Modified: 12 Jun 2013 05:32
URI: http://nal-ir.nal.res.in/id/eprint/1856

Actions (login required)

View Item View Item