发明名称 SHOCK BUMP
摘要 A shock bump comprising a diverging nose and a converging tail. The tail has at least one plan-form contour line with a pair of concave opposite sides. The shock bump provides an improved shape with relatively low drag. Furthermore, the concave shape of the tail tends to promote the development of longitudinal vortices which can reduce shock induced buffet at certain operating conditions.
申请公布号 WO2009106870(A2) 申请公布日期 2009.09.03
申请号 WO2009GB50151 申请日期 2009.02.17
申请人 AIRBUS UK LIMITED;WOOD, NORMAN 发明人 WOOD, NORMAN
分类号 B64C23/04;B64C7/00 主分类号 B64C23/04
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