Independence of helicopter rotor derivatives under non-uniformity of induced velocity distribution at low forward speed
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Independence of helicopter rotor derivatives under non-uniformity of induced velocity distribution at low forward speed
Bryce, W. W.
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https://reports.aerade.cranfield.ac.uk/handle/1826.2/4785
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A radial parabolic induced velocity distribution agreeing closely with flight measurements has been used for the hovering case. Continues...
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CoA. Reports
[280]
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