BALLISTIC DAMAGE DESIGN METHOD FOR STRUCTURE MATERIAL AND DYNAMIC COMPONENT OF AIRCRAFT

摘要

PURPOSE: A ballistic damage-resistance design method for structure material and dynamic components of an aircraft is provided to perform ballistic damage-resistance design of the structure material of the aircraft through acquisition of the ballistic damage-resistance design basic data and analysis of test result. CONSTITUTION: A ballistic damage-resistance design target item is defined (S100). Material, a tool and specimen shape are designed (S200). Bullet shot test and damage database are constructed (S300). Sizing of the structure is performed (S400). It is evaluated whether ballistic damage-resistance requirement is satisfied (S500). When the requirement is satisfied, the ballistic damage-resistance design is completed (S600). [Reference numerals] (S100) Define a ballistic damage-resistance design target item; (S200) Design material, a tool, and specimen shape; (S300) Construct a bullet shot test and damage database; (S400) Perform the sizing of the structure (analyze the damage of a ballistic damage-resistance bullet); (S500) Satisfy the requirement?; (S600) Complete the ballistic damage-resistance design