DocumentCode :
796153
Title :
NDE in aerospace-requirements for science, sensors and sense
Author :
Heyman, Joseph S.
Author_Institution :
NASA, Hampton, VA, USA
Volume :
36
Issue :
6
fYear :
1989
Firstpage :
581
Lastpage :
586
Abstract :
The complexity of modern NDE (nondestructive evaluation) arises from four main factors: quantitative measurement, science, physical models for computational analysis, realistic interfacing with engineering decisions, and direct access to management priorities. Recent advances in the four factors of NDE are addressed. Physical models of acoustic propagation are presented that have led to the development of measurement technologies advancing the ability to assure that materials and structures will perform a design. In addition, a brief discussion is given of current research for future mission needs such as smart structures that sense their own health. Such advances permit projects to integrate design for inspection into their plans, bringing NDE into engineering and management priorities. The measurement focus is on ultrasonics with generous case examples. Problem solutions highlighted include critical stress in fasteners, residual stress in steel, NDE laminography, and solid rocket motor NDE.<>
Keywords :
aerospace testing; nondestructive testing; stress measurement; ultrasonic materials testing; ultrasonic transducers; acoustic propagation; computational analysis; critical stress; interfacing; laminography; management priorities; mission needs; nondestructive evaluation; physical models; quantitative measurement; residual stress; smart structures; solid rocket motor; ultrasonics; Acoustic materials; Acoustic measurements; Acoustic propagation; Acoustic sensors; Acoustical engineering; Computational modeling; Computer interfaces; Engineering management; Physics computing; Residual stresses;
fLanguage :
English
Journal_Title :
Ultrasonics, Ferroelectrics, and Frequency Control, IEEE Transactions on
Publisher :
ieee
ISSN :
0885-3010
Type :
jour
DOI :
10.1109/58.39107
Filename :
39107
Link To Document :
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