I was wondering, how are aircraft loads transferred to the skin? that results in various failures that may occur on to the skin. like cracks for example.
Three answers:
Alpha Beta
2009-01-04 21:27:18 UTC
One of the major contributing factors is the number of times a plane is pressurized and then depressurized (which is every flight). This puts pressure on the fuselage especially with expanding and contracting as the plane ascends to altitude and descends to land. Other contributing factors can be things like corrosion.
Chris
2009-01-04 19:19:40 UTC
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In a lot of aircraft the skin of the aircraft is a main structural component of the aircraft. The primary loads on the skin are shear, bending, and tension. Most failures in the skin are seen as cracks. A lot of times it isn't the skin that falls but the rivets that holds the skin together fail.
?
2017-01-04 18:14:43 UTC
As replaced into already recognized, to stay sparkling of cracks. Cracks can devoid of difficulty improve under rigidity, particularly oscillating stresses that are shaped to the recurring pressurization and depressurization of airplane cabins. Cracks are an incredibly vast deal on airplanes. there's a useful crack length in a pressurized gadget with a objective to objective the technique to blow up i.E. The crack to propagates on the speed of sound in the medium and technique rigidity blows it up. evaluate with reference to the popping of a balloon. must you place a pinhole whilst the balloon should not be below an entire lot of tension, it won't blow up yet you get to a ingredient very immediately will it is going to violently explode. We found out approximately this the not straight forward potential in aviation. The british Comets have been exploding after X quantity of flights thinking the certainty that the spacing of the spars have been greater suitable than the imperative crack length.
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