Tytuł artykułu
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Warianty tytułu
Konferencja
Proceedings of the Fourth Seminar on Recent Research and Design Progress in Aeronautical Engineering and its Influence on Education/seminar(IV; 30.11-02.12.2000; Warszawa, Polska)
Języki publikacji
Abstrakty
The results of experimental investigations into a transonic flow of humid air over NACA0012 airfoil at a high angle of attack (5-10 deg) are presented. Three typical cases of transonic separated flows within a wide range of humidity (10% to 80%) were studied. The first one with the presence of high intensity shock causing boundary layer separation, the second one with a flow separation associated with a strong periodic shock oscillations, and the last one with a total boundary layer separation in the absence of a shock wave. For each case pressure measurements and flow visualisations have been performed.
Czasopismo
Rocznik
Tom
Strony
19--24
Opis fizyczny
Bibliogr. 5 poz., rys., wykr.
Twórcy
Bibliografia
Typ dokumentu
Bibliografia
Identyfikator YADDA
bwmeta1.element.baztech-article-PWA3-0041-0004