Passive Gust Load Alleviation In a Truss-Braced Wing Using an Inerter-Based Device
Author:
Affiliation:
1. University of Bristol
2. Airbus
Publisher
American Institute of Aeronautics and Astronautics
Link
https://arc.aiaa.org/doi/pdf/10.2514/6.2018-1958
Reference40 articles.
1. The potential of future aircraft technology for noise and pollutant emissions reduction
2. Parametric Studies of Flutter Speed in a Strut-Braced Wing
3. Structural and Aeroelastic Characteristics of Truss-Braced Wings: A Parametric Study
4. Conceptual Design Studies of a Strut-Braced Wing Transonic Transport
5. Multidisciplinary Design Optimization of Medium-Range Transonic Truss-Braced Wing Transport Aircraft
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1. Exploration of the effect of wing component post-buckling on bending-twist coupling for nonlinear wing twist;CEAS Aeronautical Journal;2022-05-25
2. Real-Time Hybrid Testing of Strut-Braced Wing Under Aerodynamic Loading Using an Electrodynamic Actuator;Experimental Techniques;2020-09-04
3. Can the inerter be a successful shock-absorber? The case of a ball-screw inerter with a variable thread lead;Journal of the Franklin Institute;2019-09
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