Add to ORKGDue to post fracture damage, the fractographic features of the rivet surfaces were completely obliterated and hence the mode of failure could not be determined. The material of the rivets and the raw material was found to conform to 30XMA specificatio
A few damaged engine components of an aircraft were forwarded to the laboratory for fractographic e...
A few components retrieved from the wreckage of a helicopter were forwarded to the laboratory for as...
Four failed components of an aeroengine were sent to the laboratory for determining the modes of fra...
Due to post fracture damage, the fractographic features of the rivet surfaces were completely oblite...
A fractured aileron connecting rod installed on an aircraft was brought to the laboratory for analys...
Examination revealed that the rivets on the sides of the bracket have failed by shear while the rive...
A broken pin assembly of an aircraft was forwarded to the laboratory for analysis. Examination reve...
This paper presents the failure analysis of a broken main wheel brake assembly of a Royal Malaysian ...
Failed brake pads of a particular type of aircraft were analyzed. The friction material and the bond...
Riveting is the most commonly used method of joining sheet metal components of the aircraft structur...
A fractured eyering shaft (port) of the cargo door assembly of an aircraft was sent to the laborator...
Fractographic study suggests that the sheet metal of the vane airfoil and the rivets failed under sh...
The main fitting subassembly of main landing gear of an aircraft was sent to the laboratory for ana...
A failed pipe fastener assembly of an aircraft was analyzed. Failure pattern suggest that the two ha...
Damaged components from an accidented aircraft were sent to the laboratory for analysis. Examination...
A few damaged engine components of an aircraft were forwarded to the laboratory for fractographic e...
A few components retrieved from the wreckage of a helicopter were forwarded to the laboratory for as...
Four failed components of an aeroengine were sent to the laboratory for determining the modes of fra...
Due to post fracture damage, the fractographic features of the rivet surfaces were completely oblite...
A fractured aileron connecting rod installed on an aircraft was brought to the laboratory for analys...
Examination revealed that the rivets on the sides of the bracket have failed by shear while the rive...
A broken pin assembly of an aircraft was forwarded to the laboratory for analysis. Examination reve...
This paper presents the failure analysis of a broken main wheel brake assembly of a Royal Malaysian ...
Failed brake pads of a particular type of aircraft were analyzed. The friction material and the bond...
Riveting is the most commonly used method of joining sheet metal components of the aircraft structur...
A fractured eyering shaft (port) of the cargo door assembly of an aircraft was sent to the laborator...
Fractographic study suggests that the sheet metal of the vane airfoil and the rivets failed under sh...
The main fitting subassembly of main landing gear of an aircraft was sent to the laboratory for ana...
A failed pipe fastener assembly of an aircraft was analyzed. Failure pattern suggest that the two ha...
Damaged components from an accidented aircraft were sent to the laboratory for analysis. Examination...
A few damaged engine components of an aircraft were forwarded to the laboratory for fractographic e...
A few components retrieved from the wreckage of a helicopter were forwarded to the laboratory for as...
Four failed components of an aeroengine were sent to the laboratory for determining the modes of fra...