Application of the Hollow-Core Optical Sensor to measurement of static structural bending

Richard D. Teichgraeber; Curtis L. Fischer; Douglas S. Abernathy; Sandra Berning

doi:10.1117/12.259795

27 November 1996 Application of the Hollow-Core Optical Sensor to measurement of static structural bending

Richard D. Teichgraeber, Curtis L. Fischer, Douglas S. Abernathy, Sandra Berning

Proceedings Volume 2838, Distributed and Multiplexed Fiber Optic Sensors VI; (1996) https://doi.org/10.1117/12.259795
Event: SPIE's 1996 International Symposium on Optical Science, Engineering, and Instrumentation, 1996, Denver, CO, United States

Abstract

An application of a linear fiberoptic sensor for detection and measurement of structural bending is described. Design, development and fabrication of the sensor is described, along with details of static bench testing and static structural bending tests of an actual aircraft wing. Knowledge of inflight aircraft surface flexure may be important for certain surveillance sensor and weapon delivery computational applications.

Citation Download Citation

Richard D. Teichgraeber, Curtis L. Fischer, Douglas S. Abernathy, and Sandra Berning "Application of the Hollow-Core Optical Sensor to measurement of static structural bending", Proc. SPIE 2838, Distributed and Multiplexed Fiber Optic Sensors VI, (27 November 1996); https://doi.org/10.1117/12.259795

ACCESS THE FULL ARTICLE

INSTITUTIONAL
Select your institution to access the SPIE Digital Library.

SELECT YOUR INSTITUTION

PERSONAL
Sign in with your SPIE account to access your personal subscriptions or to use specific features such as save to my library, sign up for alerts, save searches, etc.

PERSONAL SIGN IN

No SPIE Account? Create one

PURCHASE THIS CONTENT

SUBSCRIBE TO DIGITAL LIBRARY

50 downloads per 1-year subscription

Members: $195

Non-members: $335 ADD TO CART

25 downloads per 1 - year subscription

Members: $145

Non-members: $250 ADD TO CART

PURCHASE SINGLE ARTICLE

Includes PDF, HTML & Video, when available