Helicopter rotor blade aeroelasticity in forward flight with an implicit structural formulation
Author:
Affiliation:
1. University of Maryland, College Park, Maryland, 20742
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/3.11215
Reference17 articles.
1. 2Rosen, A., and Friedmann, P.P. "Nonlinear Equations of Equilibrium for Elastic Helicopter or Wind Turbine Blades Undergoing Moderate Deflections/' NASA CR-159478, Dec. 1978.
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