Add to ORKGAn aircraft structure is subjected to stress and fatigue during flying. Fasteners like rivets and bolts bear a large part of the stress and thus require frequent inspection for cracks around the fastener's holes. These cracks are unique in that it radial from the fastener's hole which made radiography nearly impossible in picking it up.Master of Engineering (MPE
Structural health monitoring (SHM) has been around now in research for more than 2 decades. However ...
This effort constitutes a systems engineering approach in which the materials science, ultrasound st...
The wing and body panels of modern commercial and military aircraft often consist of a three-layer s...
The work that I\u27m going to describe was funded by the Air Force Materials Lab from February 1972 ...
The detection of fatigue cracks in fastener holes in aircraft structures has been an area of concern...
As a consequence of metal fatigue, cracks can develop and grow in operational aircraft. Periodic ins...
A variety of conventional NDI techniques, such as visual inspection, radiography, eddy current and u...
ABSTRACT. In situ ultrasonic methods for structural health monitoring have the potential to provide ...
The detection of cracks below fasteners in aircraft skin has been a longstanding challenge for the a...
This paper is dealing with the ultrasonic imaging techniques and instrumentation that are used for t...
Aircraft structural components may have known “hot spots ” where any initial damage is anticipated t...
An ultrasonic inspection method was developed at FAA`s Airworthiness Assurance NDI Validation Center...
Recently, the deve1opment of a nove1 ultrasonic inspection technique that detects radial fatigue cra...
Results are presented from laboratory experiments and simulations designed to determine the ability ...
In Singapore, the Aerospace industry is one of the fastest growing industries where this expanding i...
Structural health monitoring (SHM) has been around now in research for more than 2 decades. However ...
This effort constitutes a systems engineering approach in which the materials science, ultrasound st...
The wing and body panels of modern commercial and military aircraft often consist of a three-layer s...
The work that I\u27m going to describe was funded by the Air Force Materials Lab from February 1972 ...
The detection of fatigue cracks in fastener holes in aircraft structures has been an area of concern...
As a consequence of metal fatigue, cracks can develop and grow in operational aircraft. Periodic ins...
A variety of conventional NDI techniques, such as visual inspection, radiography, eddy current and u...
ABSTRACT. In situ ultrasonic methods for structural health monitoring have the potential to provide ...
The detection of cracks below fasteners in aircraft skin has been a longstanding challenge for the a...
This paper is dealing with the ultrasonic imaging techniques and instrumentation that are used for t...
Aircraft structural components may have known “hot spots ” where any initial damage is anticipated t...
An ultrasonic inspection method was developed at FAA`s Airworthiness Assurance NDI Validation Center...
Recently, the deve1opment of a nove1 ultrasonic inspection technique that detects radial fatigue cra...
Results are presented from laboratory experiments and simulations designed to determine the ability ...
In Singapore, the Aerospace industry is one of the fastest growing industries where this expanding i...
Structural health monitoring (SHM) has been around now in research for more than 2 decades. However ...
This effort constitutes a systems engineering approach in which the materials science, ultrasound st...
The wing and body panels of modern commercial and military aircraft often consist of a three-layer s...