AU - Maleki, Gh.
AU - Tabatabaeian, S.
AU - Soltani, M.R.
AU - Davari, A.
TI - Enhancement of the Accuracy of Experimental Drag Coefficient Calculation of an Airfoil by Including the Turbulence Velocity Terms in the Wake Region
PT - JOURNAL ARTICLE
TA - mdrsjrns
JN - mdrsjrns
VO - 20
VI - 8
IP - 8
4099 - http://mme.modares.ac.ir/article-15-35184-en.html
4100 - http://mme.modares.ac.ir/article-15-35184-en.pdf
SO - mdrsjrns 8
ABĀ - In the present study, the instantaneous velocity profile behind an airfoil at two different Reynolds numbers has been measured experimentally. Data are used to study the wake profile and the corresponding drag coefficient force of the airfoil in different conditions. In the conventional and common methods for calculation of the drag force coefficient through the velocity measurement behind an airfoil, turbulence velocity terms of the momentum equation are ignored. However at moderate to high angles of attack where the flow becomes turbulent and separation occurs, the nature of the flow becomes three dimensional and disregarding the components of the fluctuation of velocity (in three dimensions) in calculation of the drag coefficient of airfoil may result in erroneous information. In the present study, in order to increase the accuracy of the experimental drag coefficient of the airfoil for moderate to high angles of attack, turbulence velocity terms in experimental drag coefficient calculation are considered and this causes an acceptable compatibility between experimental and numerical results whereas for low angles of attack, disregarding the effects of turbulence velocity terms in experimental drag coefficient calculation will improve the accuracy of the experimental drag coefficient and a desired compatibility between experimental and numerical data will be established.
CP - IRAN
IN - Department of Aerospace Engineering, Sharif University of Technology, Tehran, Iran. Postal Code: 1136511155
LG - eng
PB - mdrsjrns
PG - 2101
PT -
YR - 2020