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> Exactly how the article says they did it: They optimized the > shape of the aircraft to alter the ground-level overpressure profile > such that it minimized the perceived "loudness" of the boom at cruise > speed and altitude. (Qualitatively, it is not much different > from optimizing the shape of a boat to minimize its wake-drag.) It would be interesting to know how the drag figures varied. I notice it wasn't mentioned. Pragmatist
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