Rotation-Frequency-Driven Extension–Torsion Coupled Self-Twisting Rotor Blades
Author:
Affiliation:
1. University of Maryland, College Park, Maryland 20742
Funder
UMD VLRCOE
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
https://arc.aiaa.org/doi/pdf/10.2514/1.C034617
Reference13 articles.
1. Revitalizing Advanced Rotorcraft Research—and the Compound Helicopter: 35th AHS Alexander A. Nikolsky Honorary Lecture
2. JohnsonW.YamauchiG. K.WattsM. E. “NASA Heavy Lift Rotorcraft Systems Investigation,” NASA TP-2005-213467, Dec. 2005. doi:10.4271/2005-01-3149
3. Three-Dimensional Finite Element Formulation and Scalable Domain Decomposition for High-Fidelity Rotor Dynamic Analysis
4. Technical Notes: Hygrothermally Curvature Stable Laminates with Tension‐Torsion Coupling
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