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Damage detection and characterizatio...

Subramanian, Ajith.

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Damage detection and characterization of fiber-reinforced composites using ultrasonics.

Record Type:	Electronic resources : Monograph/item
Title/Author:	Damage detection and characterization of fiber-reinforced composites using ultrasonics./
Author:	Subramanian, Ajith.
Description:	72 p.
Notes:	Source: Masters Abstracts International, Volume: 52-01.
Contained By:	Masters Abstracts International52-01(E).
Subject:	Aerospace engineering. -
Online resource:	http://pqdd.sinica.edu.tw/twdaoapp/servlet/advanced?query=1540133
ISBN:	9781303169489

Damage detection and characterization of fiber-reinforced composites using ultrasonics.
Subramanian, Ajith.

Damage detection and characterization of fiber-reinforced composites using ultrasonics. - 72 p.

Source: Masters Abstracts International, Volume: 52-01.

Thesis (M.S.)--Iowa State University, 2013.

Due to the prevalence of fiber-reinforced composites in industrial applications, the need for damage-detection and characterization has increased. Ultrasonic nondestructive testing (NDT) is a powerful and non-invasive method of detecting flaws and defects in composite materials. Air-coupled and immersion UT techniques are used to quantify the effect of matrix microcracking and delamination within the composite laminate. Detection of matrix microcracks in the laminate is of primary concern since microcracking is one of the initial damage modes resulting in local stiffness reduction. The techniques considered include pulse-echo in immersion, angle-beam through-transmission Lamb wave time-of-flight shift and velocity measurements, and angle-beam backscatter measurements from single microcracks within the composite laminate. The time-of-flight measurements are shown to be a reasonable method for quantifying stiffness reduction in the laminate, however special attention must be provided to the Lamb modes considered and their sensitivity to the independent stiffness components. The angle-beam backscatter technique may be used to detect individual microcracks but poses a limitation on the frequency and depth of inspection. Ultimately, the quantification of microcracking will provide an early descriptor of failure in the laminate.

ISBN: 9781303169489Subjects--Topical Terms:

1002622
Aerospace engineering.

Damage detection and characterization of fiber-reinforced composites using ultrasonics.
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020 $a 9781303169489
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100 1 $a Subramanian, Ajith. $3 3184814
245 1 0 $a Damage detection and characterization of fiber-reinforced composites using ultrasonics.
300 $a 72 p.
500 $a Source: Masters Abstracts International, Volume: 52-01.
500 $a Adviser: Vinay Dayal.
502 $a Thesis (M.S.)--Iowa State University, 2013.
520 $a Due to the prevalence of fiber-reinforced composites in industrial applications, the need for damage-detection and characterization has increased. Ultrasonic nondestructive testing (NDT) is a powerful and non-invasive method of detecting flaws and defects in composite materials. Air-coupled and immersion UT techniques are used to quantify the effect of matrix microcracking and delamination within the composite laminate. Detection of matrix microcracks in the laminate is of primary concern since microcracking is one of the initial damage modes resulting in local stiffness reduction. The techniques considered include pulse-echo in immersion, angle-beam through-transmission Lamb wave time-of-flight shift and velocity measurements, and angle-beam backscatter measurements from single microcracks within the composite laminate. The time-of-flight measurements are shown to be a reasonable method for quantifying stiffness reduction in the laminate, however special attention must be provided to the Lamb modes considered and their sensitivity to the independent stiffness components. The angle-beam backscatter technique may be used to detect individual microcracks but poses a limitation on the frequency and depth of inspection. Ultimately, the quantification of microcracking will provide an early descriptor of failure in the laminate.
590 $a School code: 0097.
650 4 $a Aerospace engineering. $3 1002622
650 4 $a Engineering. $3 586835
650 4 $a Mechanics. $3 525881
690 $a 0538
690 $a 0537
690 $a 0346
710 2 $a Iowa State University. $b Engineering Mechanics. $3 3184815
773 0 $t Masters Abstracts International $g 52-01(E).
790 $a 0097
791 $a M.S.
792 $a 2013
793 $a English
856 4 0 $u http://pqdd.sinica.edu.tw/twdaoapp/servlet/advanced?query=1540133