Hello, I had previously looked at the reference you gave, but even though I understand what you did I still don't know why would Fty*Agross is equal to sigma*Anet. Yes, the force equation was made to be equal to yield, but why is it equal to sigma*Anet? When finding yield stress, is it found...
Hello first of all thank you very much for all the answers but is there a reference where this formula is written? or did you reach it from a ratio-proportion calculation? In other words, do we reach your formula when Fty*Agross=sigma*Anet and then t's cancel each other out?
Hello,
I was reading dta guidelines about small antenna installation on top of the fuselage from Patrick Safarian and ı came across a problem and ı couldn't solve it. Can you help me about this?
"If deltaP=8.9 psi, fuselage Radius=128", pitch(spacing)=1.2", hole diameter=0.188", t=0.062"...
Hello,
I was reading dta guidelines about small antenna installation on top of the fuselage from Patrick Safarian and ı came across a problem and ı couldn't solve it. Can you help me about this?
"If deltaP=8.9 psi, fuselage Radius=128", pitch(spacing)=1.2", hole diameter=0.188", t=0.062"...
It says same things "For multi-load path, indeterminate structures, the airplane support structure stiffness can have astrong influence and therefore, the stiffness as well as the geometry should be simulated." but why is it because of deflections? why does stiffness strong influence when...
It's not just about creating tests or analytics, it's about both at the same time because both need to have the same assumptions as much as possible. Boeing D6-55441 document says that if your structure is determinate then rigid fixture is enough for both testing analyzing but otherwise you need...
Hello everyone,
I'm currently working on a structural analysis for an aircraft cabin interior furnishing. In my research, I came across guidance in the Boeing D6-55441 document that discusses test fixture validation and the determination of whether a component should be modeled/tested using a...
