A) There are two steel plates which are is part of aeroplane
body as shown in Figure 6(a) are
to be joint together by means of lap joint as shown in
Figure6(b) by two steel rivets of
diameter and load as given in table below.
Calculate the following:
1) Shearing area of the rivets
2) The allowable shear stress in rivets
3) The factor of safety in operation if ultimate shear stress
210MPa.
A There Are Two Steel Plates Which Are Is Part Of Aeroplane Body As Shown In Figure 6 A Are To Be Joint Together By Me 1 (82.47 KiB) Viewed 40 times
A There Are Two Steel Plates Which Are Is Part Of Aeroplane Body As Shown In Figure 6 A Are To Be Joint Together By Me 2 (3.06 KiB) Viewed 40 times
Riveted Lap Joint (Top View) Riveted Lap Joint (Side View) Figure 6(b). Single Lap joint
Diameter(mm) Load(KN) Trainee Number 20191563 5 50
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