Dynamic wing shape sensing during wind tunnel test using optical fiber distributed and point sensing technologies

S. Shoham; U. Ben-Simon; I. Kressel; M. Rattner; M. Freydin; D. Raveh; S. Sheinkman; M. Tur

Dynamic wing shape sensing during wind tunnel test using optical fiber distributed and point sensing technologies

S. Shoham, U. Ben-Simon, I. Kressel, M. Rattner, M. Freydin, D. Raveh, S. Sheinkman, M. Tur

Aerospace Engineering

Research output: Contribution to conference › Paper › peer-review

Abstract

Optical Fiber based point and distributed strain sensing techniques were applied on a specially designed, ULTEM-9085, rapid prototyping wing. The deformed shape of the wing was measured in real time under both prescribed bending and torsion loading followed by dynamic wind tunnel test. The strain to displacements algorithm used was found to be highly suitable for aeroelastic shape sensing.

Original language	English
Pages	1469-1474
Number of pages	6
State	Published - 2018
Event	58th Israel Annual Conference on Aerospace Sciences, IACAS 2018 - Tel-Aviv and Haifa, Israel Duration: 14 Mar 2018 → 15 Mar 2018

Conference

Conference	58th Israel Annual Conference on Aerospace Sciences, IACAS 2018
Country/Territory	Israel
City	Tel-Aviv and Haifa
Period	14/03/18 → 15/03/18

ASJC Scopus subject areas

Aerospace Engineering
Space and Planetary Science

UN SDGs

This output contributes to the following UN Sustainable Development Goals (SDGs)

Cite this

@conference{6bd39f2cec5b4304ad89c9d8fee8ee08,

title = "Dynamic wing shape sensing during wind tunnel test using optical fiber distributed and point sensing technologies",

abstract = "Optical Fiber based point and distributed strain sensing techniques were applied on a specially designed, ULTEM-9085, rapid prototyping wing. The deformed shape of the wing was measured in real time under both prescribed bending and torsion loading followed by dynamic wind tunnel test. The strain to displacements algorithm used was found to be highly suitable for aeroelastic shape sensing.",

author = "S. Shoham and U. Ben-Simon and I. Kressel and M. Rattner and M. Freydin and D. Raveh and S. Sheinkman and M. Tur",

note = "Publisher Copyright: {\textcopyright} 2018 Israel Annual Conference on Aerospace Sciences. All rights reserved.; 58th Israel Annual Conference on Aerospace Sciences, IACAS 2018 ; Conference date: 14-03-2018 Through 15-03-2018",

year = "2018",

language = "אנגלית",

pages = "1469--1474",

}

TY - CONF

T1 - Dynamic wing shape sensing during wind tunnel test using optical fiber distributed and point sensing technologies

AU - Shoham, S.

AU - Ben-Simon, U.

AU - Kressel, I.

AU - Rattner, M.

AU - Freydin, M.

AU - Raveh, D.

AU - Sheinkman, S.

AU - Tur, M.

PY - 2018

Y1 - 2018

N2 - Optical Fiber based point and distributed strain sensing techniques were applied on a specially designed, ULTEM-9085, rapid prototyping wing. The deformed shape of the wing was measured in real time under both prescribed bending and torsion loading followed by dynamic wind tunnel test. The strain to displacements algorithm used was found to be highly suitable for aeroelastic shape sensing.

AB - Optical Fiber based point and distributed strain sensing techniques were applied on a specially designed, ULTEM-9085, rapid prototyping wing. The deformed shape of the wing was measured in real time under both prescribed bending and torsion loading followed by dynamic wind tunnel test. The strain to displacements algorithm used was found to be highly suitable for aeroelastic shape sensing.

UR - http://www.scopus.com/inward/record.url?scp=85048980903&partnerID=8YFLogxK

M3 - ???researchoutput.researchoutputtypes.contributiontoconference.paper???

AN - SCOPUS:85048980903

SP - 1469

EP - 1474

T2 - 58th Israel Annual Conference on Aerospace Sciences, IACAS 2018

Y2 - 14 March 2018 through 15 March 2018

ER -

Dynamic wing shape sensing during wind tunnel test using optical fiber distributed and point sensing technologies

Abstract

Conference

ASJC Scopus subject areas

UN SDGs

Other files and links

Fingerprint

Cite this