Anand, Shreyas and Pandey, Akshay and Sharma, Arpita and Kini, Chandrakant R (2017) Effect of trailing edge roundness on fx 63-137 And selig s1223 airfoil. ARPN Journal of Engineering and Applied Sciences, 12 (19). pp. 5494-5499. ISSN 1819-6608
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Abstract
Wortmann FX 63-137 and Selig S1223 are high lift low Reynolds Number Airfoils which have widespread applications in heavy lift cargo planes and student projects like FSAE. The trailing edge is often given a radius for the ease of manufacturing and safety. This paper studies the variation in lift coefficients, drag coefficients and aerodynamic efficiency because of the amendments in the trailing edge radii of these two airfoils, ranging from 0.25% to 1.5% of the chord length
Item Type: | Article |
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Uncontrolled Keywords: | airfoil, trailing edge radius, high Lift, Selig S1223, wortmann FX 63-137, chord, computational fluid dynamics. |
Subjects: | Engineering > MIT Manipal > Aeronautical and Automobile |
Depositing User: | MIT Library |
Date Deposited: | 10 Nov 2017 09:23 |
Last Modified: | 10 Nov 2017 09:23 |
URI: | http://eprints.manipal.edu/id/eprint/149934 |
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