Wing Shape Sensing from Measured Strain-Reference-Cited by-同舟云学术

Wing Shape Sensing from Measured Strain

Published:2016-03 Issue:3 Volume:54 Page:1068-1077
ISSN:0001-1452
Container-title:AIAA Journal
language:en
Short-container-title:AIAA Journal

Author:

Pak Chan-gi¹

Affiliation:

1. NASA Armstrong Flight Research Center, Edwards, California 93523-0273

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Aerospace Engineering

Link

http://arc.aiaa.org/doi/pdf/10.2514/1.J053986

Reference14 articles.

1. NollT. E.BrownJ. M.Perez-DavisM. E.IshamaelS. D.TiffanyG. C.GaierM. “Investigation of the Helios Prototype Aircraft Mishap, Volume I Mishap Report,” NASA, Washington, D.C., 2004, https://www.nasa.gov/pdf/64317main_helios.pdf.

2. LizotteA. M.LokosW. A. “Deflection-Based Structural Loads Estimation from the Active Aeroelastic Wing F/A-18 Aircraft,” NASA TM-2005-212871, 2005.

3. Dynamic strain measurements by fibre Bragg grating sensor

4. KoW. L.RichardsW. L.TranV. T. “Displacement Theories for In-Flight Deformed Shape Predictions of Aerospace Structures,” NASA TP-2007-214612, 2007.

5. Estimation of dynamic structural displacements using fiber Bragg grating strain sensors

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