Does anyone know, In Bolt Group Analysis Page D1.14 Bruhn, why there is a value Zero added to the Componenet Bolt (C) load equations.
Sum H = 250 + 120x1/1.25 + 0 = 346 lb
Sum V = 250 + 120x.75/1.25 + 0 = -122 lb
Is this a mistake print error or does it mean anything ?
Hi Guys
Does anyone know where I can get the data sheets to find the Insert Pullout strength through the Honeycomb panel with composite facing skins, ESA document is currently under review.
Thanks in advance
A report refers to:
From classical laminate analysis theory
Fs=3M/2Rbt
where M is the applied bending moment
R is radius of curvature
b is plate width
t is plate thickness
Can someone help me to find the source of the equation.
Could anyone please let me know, if you have any techincal information:
I have a window manufactured from Acrylic (MIL-P-5425) mounted to door frame manufactured from composite (7 layers of Carbon Fibre 199-45-005, Type A, Style 5H),) by using rubber seal (A-A-59588A Class 1A),
55 knots gust...
