Damage Assessment of Structures - An Air Force Office of Scientific Research Structural Mechanics Perspective-Reference-Cited by-同舟云学术

Damage Assessment of Structures - An Air Force Office of Scientific Research Structural Mechanics Perspective

Published:2007-09 Issue: Volume:347 Page:69-74
ISSN:1662-9795
Container-title:Key Engineering Materials
language:
Short-container-title:KEM

Author:

Giurgiutiu Victor¹

Affiliation:

1. Air Force Office of Scientific Research

Abstract

This paper presents the perspective of the Structural Mechanics program of the Air Force Office of Scientific Research on the damage assessment of structures. It is found that damage assessment of structures plays a very important role in assuring the safety and operational readiness of Air Force fleet. The current fleet has many aging aircraft, which poses a considerable challenge for the operators and maintainers. The nondestructive evaluation technology is rather mature and able to detect damage with considerable reliability during the periodic maintenance inspections. The emerging structural health monitoring methodology has great potential, because it will use on-board damage detection sensors and systems, will be able to offer on-demand structural health bulletins. Considerable fundamental and applied research is still needed to enable the development, implementation, and dissemination of structural health monitoring technology.

Publisher

Trans Tech Publications, Ltd.

Subject

Mechanical Engineering,Mechanics of Materials,General Materials Science

Link

https://www.scientific.net/KEM.347.69.pdf

Reference8 articles.

1. Air Force Office of Scientific Research public website http: /www. afosr. af. mil/home. htm.

2. Keating, E. G.; Dixon, M.: Investigating Optimal Replacement of Aging Air Force Systems, ISBN 0-8330-3483-9, Rand Corporation, Santa Monica, CA, (2003).

3. Keating, E. G.; Snyder, D.; Dixon, M.; Loredo, E. N.: Aging Aircraft Repair-Replacement Decision with Depot Level Capacity as a Policy Choice Variable, ISBN 0-8330-3692-0, Rand Corporation, Santa Monica, CA, (2005).

4. Bruhn, E. F.: Analysis and Design of Flight Vehicle Structures, Jacobs Publishing, Inc., (1973).

5. Wood, H. A.: Fracture Control Procedures for Aircraft Structural Integrity, AFFDL Report TR-2-89, WPAFB, Ohio, July (1971).

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