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NTIS 바로가기Bulletin of the JSME, v.27 no.232=no.232, 1984년, pp.2107 - 2112
Fujita, Hajime (Hitachi Ltd, Mechanical Engineering Research Lab, Tsuchiura, Jpn) , Takada, Yoshihiro , Satoh, Shigenori
Flow around a flat delta wing is investigated in order to establish a technique of visualization of three-dimensional flow by smoke wire method, considering application to the study of steady and non-steady responses of single and cascades of delta wings. It is found that the structure of the leading-edge vortices, in particular reference to the breakdown of the vortex core over the wing surface as well as the structure of the free vortex zone can be investigated in detail by choosing proper combinations of relative attitudes and locations between the wind and the smoke wire, and taking photographs from three perpendicular directions.
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