green66
Jun 11, 2004, 07:48 AM
Hi all,
Concerning sheeted foam wings --- Is there a practical way, or accepted rule of thumb, to determine the required compressive modulus of the foam to avoid bending-induced buckling of the top sheeting? I know the wing's thickness, sheeting thickness / properties, and anticipated bending moment.
Thanks in advance.
Concerning sheeted foam wings --- Is there a practical way, or accepted rule of thumb, to determine the required compressive modulus of the foam to avoid bending-induced buckling of the top sheeting? I know the wing's thickness, sheeting thickness / properties, and anticipated bending moment.
Thanks in advance.