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• Published Open access Original Research Special issue 29 Mar 2024

  Study on a Supercritical Airfoil with Variation in Thickness for Improved Aerodynamic Characteristics in Transonic Regime

  By Siddalingappa P. Kodigaddi, Mohammed Ayaan Khazi, Mounika C.S., Deva N., Sangeetha Patil P., Yathish R., Somashekar V.

  Abstract: In this research the steady state analysis of a supercritical airfoil is done to understand the flow physics at transonic Mach number regime for various thickness. The modeling of NASA SC (2) 0714 supercritical airfoil with various thickness values is done. The steady state analysis is carried out for different test cases in combination with different thickness, angle of attack and Mach number at 10 km altitude using density-based Reynolds …

  Published in Journal of Polymer & Composites · Vol. 11, Issue 13, 2023 · pp. 122–134 Read article →