Study on damage of a reinforced aircraft skin subjected to 12.7 mm projectile impact;

In order to validate its enhancement effect comparing to traditional bond structures,two groups of stitched/non-stitched composite T-shaped and L-shaped skin-to-stiffener performs were designed,and check experiment on the strength of non-stitched/stitched skin-to-stiffener structures,loaded in tensile pull-off,was performed.

Loading trajectory is the key factor for aircraft skin stretch forming.

Based on the characteristic analysis of infrared radiation sources on jet aircraft, an engineering calculation algorithm was proposed to calculate the infrared radiation about jet engine, tail flame, and aircraft skin of jet aircraft.

Research on optimizations of patch shape for bonding repair of aircraft skin;

Applying prestressing welding technique to locomotive skin;

A method for approximate NURBS skinning;

In terms of the fact that Skinned Mesh Animations(SMA) based on Matrix palette skinning(MPS) does not work well for non-quasi-articulated objects, this paper presents a new technology for skin deformation,skinning arbitrary deformation,which can set proxy-joints,automatically construct skinning approximations for arbitrary precomputed animations,and use dual quaternion for skinning.

Comparing with traditional method of skinning curves, it uses data re-sampling technique successfully, solving problems as twist in some complex area, avoiding generating huge amounts of control points.