Aerodynamic structure with asymmetrical shock bump

B - Operations – Transporting – 64 – C

Patent

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Details

B64C 23/04 (2006.01)

Patent

CA 2713359

An aerodynamic structure comprising a shock bump (3) extending from its surface. The shock bump is asymmetrical about a plane of asymmetry, and the plane of asymmetry: passes through a centre (6) of the shock bump, is parallel with a principal direction of air flow over the structure, and extends at a right angle to the surface ofthe structure.

La présente invention concerne une structure aérodynamique comportant à sa surface une bosse antichoc. La bosse antichoc est asymétrique autour d'un plan d'asymétrie et ce plan d'asymétrie passe par un centre de la bosse antichoc, est parallèle à une direction principale d'écoulement d'air sur la structure et s'étend perpendiculairement à la surface de la structure.

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