Real Time Measurement of Airplane Flutter via Distributed Acoustic Sensing

Author:

Bakhoum Ezzat G.ORCID,Zhang Cheng,Cheng Marvin H.

Abstract

This research group has recently used the new technology Distributed Acoustic Sensing (DAS) for the monitoring and the measurement of airplane flutter. To the authors’ knowledge, this is the first such use for this new technology. Traditionally, the measurement of airplane flutter requires the mounting of a very large number of sensors on the wing being monitored, and extensive wiring must be connected to all these sensors. The new system and technology introduced in this paper dramatically reduces the hardware requirements in such an application: all the traditional sensors and wiring are replaced with one fiber optic cable with a diameter of 2 mm. An electro-optical system with the size of a desktop PC monitors simultaneously one or more of such fiber optic cables and detects/characterizes any mechanical disturbances on the cables. Theoretical and experimental results are given.

Publisher

MDPI AG

Subject

Aerospace Engineering

Reference21 articles.

1. Introduction to Aircraft Aeroelasticity and Loads;Wright,2007

2. An introductory guide to literature in aeroelasticity

3. Robust Aeroservoelastic Stability Analysis;Lind,1999

4. Flutterometer: An On-Line Tool to Predict Robust Flutter Margins

5. Acceleration Measurement;Sydenham,2005

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