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An aircraft wing oscillates under wind gusts. The oscillations are expected to be at about 2 Hz. Wing-mounted strain gauge sensors are connected to a +-5 V, 12-bit A/D converter and a data acquisition system to measure this. For each test block, 10 seconds are sampled. Suggest an appropriate sample rate?​

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An aircraft wing oscillates under wind gusts. The oscillations are expected to be at about 2 Hz. Win...
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