发明名称 CORPO AERODINAMICO PROVVISTO DI CAVITA' SUPERFICIALI.
摘要 An airfoil is provided with a surface cavity (1) having an aperture (2), towards the external surface of the airfoil, and defined by a front edge (7) and rear edge (6) positioned transversally to the direction of movement of the profile, in which the front edge (7) is reentrant with respect to the rear edge (6) by a distance (H). The area (5) located upstream of the front edge (7) slopes gradually downwards from the outer surface of the profile towards the cavity (1) in order to divert part of the flow of the fluid F, which skims the outer surface, into the cavity (1).
申请公布号 ITRM20010501(D0) 申请公布日期 2001.08.10
申请号 IT2001RM00501 申请日期 2001.08.10
申请人 UNIVERSITA' DEGLI STUDI DI ROMA LA SAPIENZA 发明人 GAMMA FAUSTO;SCIUBBA ENRICO;ZINGARO DOMENICO
分类号 B64C23/00 主分类号 B64C23/00
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