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Aerodynamic structure with series of shock bumps
Aerodynamic structure with series of shock bumps
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机译:具有一系列减震器的空气动力学结构
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摘要
An aerodynamic structure (1) comprising a series of shock bumps (3a, 3b, 3c) extending from its surface. The shock bumps are distributed along a line (7) with a smaller mean angle of sweep than an unperturbed shock (4) which would form adjacent to the surface during transonic movement of the structure in the absence of the shock bumps. Instead of being distributed along the line of the unperturbed shock, the shock bumps are distributed along a line which is less swept than the mean angle of sweep of the unperturbed shock. When the structure is moved at a transonic speed; a shock forms adjacent to its surface and the shock bumps perturb the shock (9) so as to reduce its angle of sweep.
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机译:包含一系列减震块( 3 B> a I> ,3 B> b <的气动结构( 1 B>) / I> ,3 B> c I>)从其表面延伸。冲击凸点沿线( 7 B>)分布,其平均后掠角小于未扰动冲击( 4 B>),后者在跨子跨音速运动时会与表面相邻没有冲击波的结构。冲击隆起不是沿着未扰动的冲击线分布,而是沿着比未扰动的冲击的平均后掠角小的扫掠线分布。当结构以跨音速移动时;会在其表面附近形成冲击,并且冲击凸点会扰动冲击( 9 B>),以减小其后掠角。
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