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  1. E

    Fracture Mechanics - Residual Strength/Crack Propagation

    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"...
  2. E

    Fracture Mechanics - Residual Strength

    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"...
  3. E

    statically determinate and indeterminate aircraft structure

    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...

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