Effect of trailing edge roundness on FX 63-137 and Selig S1223 Airfoil

Shreyas Anand; Akash Pandey; Arpit Sharma; Chandrakant R. Kini

Effect of trailing edge roundness on FX 63-137 and Selig S1223 Airfoil

Shreyas Anand, Akash Pandey, Arpit Sharma, Chandrakant R. Kini

Department of Aeronautical and Automobile Engineering, Manipal Institute of Technology, Manipal

Research output: Contribution to journal › Article › peer-review

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.

Original language	English
Pages (from-to)	5494-5499
Number of pages	6
Journal	ARPN Journal of Engineering and Applied Sciences
Volume	12
Issue number	19
Publication status	Published - 01-10-2017

All Science Journal Classification (ASJC) codes

Engineering(all)

Cite this

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AB - 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.

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Effect of trailing edge roundness on FX 63-137 and Selig S1223 Airfoil

Abstract

All Science Journal Classification (ASJC) codes

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