ANALYSIS OF TRANSONIC FLOW PAST CUSPED AIRFOILS
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České vysoké učení technické v Praze
Czech Technical University in Prague
Czech Technical University in Prague
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Transonic flow past two cusped airfoils is numerically solved and achieved results are analyzed by means of flow behavior and oblique shocks formation.Regions around sharp trailing edges are studied in detail and parameters of shock waves are solved and compared using classical shock polar approach and verified by reduction parameters for symmetric configurations.
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Acta Polytechnica. 2015, vol. 55, no. 3, p. 193-198.
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Except where otherwised noted, this item's license is described as Creative Commons Attribution 4.0 International License