Application of the finite-state arbitrary-motion aerodynamics to rotor blade aeroelastic response and stability in hover and forward flight
Author:
Affiliation:
1. Hughes Helicopters, Inc., Culver City; California, University, Los Angeles, CA
2. California, University, Los Angeles, CA
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.1985-763
Reference26 articles.
1. tary-wing Aeroelasticity:' Journal of Aircraft, Vol. 14, No. 11, November 1977, pp. 1027-1041. * Dinyavari, M.A.H., and Friedmann, P.P."Un' steady Aerodynamics in Time and Frequency
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