Hello,
while designing a unloaded bracket, client has provided a current requirement as 30 Amperes. based on the current, I need to select rivet size and no of rivets. for example, 30 Amperes current, I can go with 3 rivets with 4.8 mm diameter fastener or 4 rivets with 4 mm diameter...
Hello all,
Is there any books to refer for aerospace metallic materials.. MMPDS is getting difficult to understand.. any simpler book with MMPDS content ?
Thanks
Based on bending + compression + buckling which type of stringer cross section is most preferred for aircraft wing and fuselage ? C or T or L or J or I or hat or inverted hat section..
When do we use von mises stress and max principal stress in analyzing aerostructures? I got to know based on ductile and brittle materials we use.. but is there any other criteria to use. when subjected to tension compression or bending loads ? Which stress do we use or consider as critical ...
Why can't we use steel as Qing skin instead of aluminum alloy 2024.. although skin is lighter in weight when compared to aluminum alloy 2024.. density of steel is more than aluminum alloy.. is there any engineering reason ( tensile or compression ) other material properties to use aluminum alloy...
Hello all,
Could you please let me know the significance of area moment of inertia while doing aircraft structural analysis ( eg beam analysis) And also practical importance of MOI..
Thanks
Regards
Manjunathca
