The solid cylinders exhibited a faster percentage mass loss than all porous scaffolds.
Not all the backward inclined cylinders exhibit crosswind responses smaller than those of the vertical cylinder does.
The present study presents the finite element modeling procedure of two composite laminated cylinders exhibiting initial geometric imperfections.
NiO nanostructured cylinders exhibit a relatively high specific surface area around 130 m2/g and a pore size around 4 nm, consistent with the observed nanostructure.
The present investigations of mold-cast and melt-spun Nd60FexCo30-xAl10 samples show that the Fe-rich as-cast (x=7.5, 10) bulk cylinders exhibit a partially crystalline structure, whereas the melt-spun ribbons and Co-rich as-cast bulk cylinders are amorphous.
The static aerodynamic force on the cylinder exhibits reattachment, which lowers the drag coefficient and increases the lift coefficient at the critical Reynolds number.
Experimental results showed that the flow structures around the square cylinder exhibit three modes leading-edge separation, separation bubble and attached flow.
On the other hand, the graphene with Pt cylinder array exhibited better macrotribological performance because Pt cylinders had certain pinning effects on graphene sheets and prevented graphene sheets from slipping.
The methods proposed were validated by performing elastic plastic finite element analyses of a smooth cylinder that exhibited Bree-type ratcheting.
The step response characteristics shows that interconnected pneumatic cylinders system exhibits 13.8% more rise time but the overshoot is reduced 28.8% compared to conventional single cylinder servo pneumatic system with supply pressure 0.6 MPa.
