Real-Time Hybrid Testing of Strut-Braced Wing Under Aerodynamic Loading Using an Electrodynamic Actuator-Reference-Cited by-同舟云学术

Real-Time Hybrid Testing of Strut-Braced Wing Under Aerodynamic Loading Using an Electrodynamic Actuator

Published:2020-09-04 Issue:6 Volume:44 Page:821-835
ISSN:0732-8818
Container-title:Experimental Techniques
language:en
Short-container-title:Exp Tech

Author:

Ruffini V.,Szczyglowski C.,Barton D. A. W.,Lowenberg M.,Neild S. A.

Funder

Engineering and Physical Sciences Research Council

Publisher

Springer Science and Business Media LLC

Subject

Mechanical Engineering,Mechanics of Materials

Link

https://link.springer.com/content/pdf/10.1007/s40799-020-00394-5.pdf

Reference46 articles.

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3. Bradley MK, Droney CK, Allen TJ (2015) Subsonic ultra green aircraft research. Phase II - Volume I; Truss braced wing design exploration, Tech. Rep. NASA-CR-2015-218704/VOL1, NASA

4. Turriziani RV, Lovell WA, Martin GL, Price JE, Swanson EE, Washburn GF (1980) Preliminary design characteristics of a subsonic business jet concept employing an aspect ratio 25 strut braced wing, Tech. Rep. NASA-CR-159361 NASA

5. Szczyglowski C, Neild S, Titurus B, Jiang J, Cooper J, Coetzee E (2017) Passive gust loads alleviation in a truss-braced wing using integrated dampers. In: 17th International Forum on Aeroelasticity and Structural Dynamics, IFASD 2017

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