Numerical Investigations on Unsteady Features of Rounded Trailing Edge Airfoils

<div>Comparison of <svg height="9.5404pt" id="M103" style="vertical-align:-0.2324991pt" version="1.1" viewbox="-0.0498162 -9.3079 20.5079 9.5404" width="20.5079pt" xmlns="http://www.w3.org/2000/svg" xmlns:xlink="http://www.w3.org/1999/xlink"><g transform="matrix(.013,0,0,-0.013,0,0)"><path d="M600 0V24L339 665L311 657L43 24V0H600ZM497 50H107L303 539L497 50Z"></path></g><g transform="matrix(.013,0,0,-0.013,8.327,0)"><path d="M614 175C564 76 510 21 408 21C256 21 146 149 146 336C146 488 235 629 402 629C510 629 570 586 597 480L626 488C620 541 614 582 606 638C578 643 510 665 429 665C206 665 44 527 44 316C44 157 153 -15 402 -15C474 -15 558 5 586 11C604 45 629 119 643 165L614 175Z"></path></g><g transform="matrix(.013,0,0,-0.013,17.037,0)"><path d="M238 0V26C174 32 166 38 166 104V712C132 700 70 683 18 677V653C81 647 87 645 87 577V104C87 38 78 32 15 26V0H238Z"></path></g></svg> for two airfoils.</div>

International Journal of Aerospace Engineering

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Figure 17

Figure 17: Numerical Investigations on Unsteady Features of Rounded Trailing Edge Airfoils 