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Prasad et al., 2012 - Google Patents

Finite state inflow models for a coaxial rotor in hover

Prasad et al., 2012

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Document ID
10821641606857342675
Author
Prasad J
Nowak M
Xin H
Publication year

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Formation of a robust, accurate, and computationally efficient induced inflow model is needed to support real time coaxial rotorcraft simulations. Two generalized coaxial rotor models are developed to handle hovering flight condition. One inflow model is obtained by …
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