Hello,
I have a composite panel (AL core 1.89" and AL face sheet 0.032" bonded with BMS 5-101, Type I, Grade 10) to be used on attendant partition with a 2 disbondings between core and face sheet. The disbonding size is 2” X 9” one away from edge and other disbonding of similar size near edge...
Hello All,
I am using FEMAP NX NASTRAN 9.3. Currently I am working on finite modelling of class divider and it is with dog house. I was wondering if anyone of you know how to get the joint loads between partition and doghouse? Please see attached for the picture and clarification of my problem...
Hello All,
Question:
I have a tensile modulus for a face sheet of honeycomb panel which is composed of 6 layers of phenolic (0/90/0/90/0/90). And I would like to calculate tensile modulus for individual layer. Is there any formula which calculates it?
OR
If I know value of modulus for an...
Hi,
I am very green to this stress analysis field and I am hoping to get guidance from this forum.
I am doing 777 floor panel strength substantiation. Floor panel material BMS4-20 Type III. Loading is console load from seats which in Z direction. For conservative analysis I am considering it as...