Open AccessANALYSIS OF TRANSONIC FLOW PAST CUSPED AIRFOILS
Author(s) -
Jiří Stodůlka,
Pavel Šafařík
Publication year - 2015
Publication title -
acta polytechnica
Language(s) - English
Resource type - Journals
SCImago Journal Rank - 0.207
H-Index - 15
eISSN - 1805-2363
pISSN - 1210-2709
DOI - 10.14311/ap.2015.55.0193
Subject(s) - transonic , airfoil , mechanics , shock wave , shock (circulatory) , oblique shock , flow (mathematics) , oblique case , physics , mathematics , aerodynamics , geology , medicine , linguistics , philosophy
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.