Study of Transonic Cascade Airfoils by a Panel Method

A panel method was applied to transonic flow problems of obtaining shock-free airfoils in turbomachine cascades. With introduction of Sovieczky's fictitious gas concept, the panel method succeeded in treating both subsonic and supersonic flow regions in a unified fashion. It was shown that the...

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Veröffentlicht in:	Nihon Kikai Gakkai rombunshuu. B hen 1986/12/25, Vol.52(484), pp.3880-3887
Hauptverfasser:	SATO, Iwataro, KAJI, Shojiro
Format:	Artikel
Sprache:	eng ; jpn
Schlagworte:	Turbomachine
Online-Zugang:	Volltext
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