发明名称 Boundary layer control of aerodynamic airfoils
摘要 Boundary layer control of a structural element in fluid stream is achieved by the following operations: providing in such structural element at least one region equipped with micro porous structure by an electroforming technique; having a fluid stream flow through the external surface of the said at least one region, inwards or outwards with respect to the environment in which that element is placed.
申请公布号 GB9927807(D0) 申请公布日期 2000.01.26
申请号 GB19990027807 申请日期 1999.11.24
申请人 BATTISTI, LORENZO 发明人
分类号 B64C21/02;B64C21/04;B64C21/06;C25D1/08;F01D5/14;F01D5/18;F01D25/12;F04D29/32;F04D29/68 主分类号 B64C21/02
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