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

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

Research output: Contribution to journalArticle

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 languageEnglish
Pages (from-to)5494-5499
Number of pages6
JournalARPN Journal of Engineering and Applied Sciences
Volume12
Issue number19
Publication statusPublished - 01-10-2017

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Airfoils
Drag coefficient
Aerodynamics
Reynolds number
Students

All Science Journal Classification (ASJC) codes

  • Engineering(all)

Cite this

Anand, Shreyas ; Pandey, Akash ; Sharma, Arpit ; Kini, Chandrakant R. / Effect of trailing edge roundness on FX 63-137 and Selig S1223 Airfoil. In: ARPN Journal of Engineering and Applied Sciences. 2017 ; Vol. 12, No. 19. pp. 5494-5499.
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Effect of trailing edge roundness on FX 63-137 and Selig S1223 Airfoil. / Anand, Shreyas; Pandey, Akash; Sharma, Arpit; Kini, Chandrakant R.

In: ARPN Journal of Engineering and Applied Sciences, Vol. 12, No. 19, 01.10.2017, p. 5494-5499.

Research output: Contribution to journalArticle

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