ANALYSIS OF TRANSONIC FLOW PAST CUSPED AIRFOILS

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...

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Bibliographic Details
Main Authors: Jiří Stodůlka, Pavel Šafařík
Format: Article
Language:English
Published: CTU Central Library 2015-06-01
Series:Acta Polytechnica
Subjects:
Online Access:https://ojs.cvut.cz/ojs/index.php/ap/article/view/2297