The principal modifications are as follows:the flight g-load is improved from 7g to 8g or larger in order to enhance the maneuver performance of flight;the action radius is raised from xxx km to xxxx km and above;the store stations on a lower surface of the wing are increased to 8 positions.

Numerical and Experimental Investigation on Penetration Effects of Semi-Armor-Piercing Warhead;

Based on the research experience of semi-armor-piercing warhead,integrated design method for SAPW was studied by advanced engineering design method and computer technique.

The head thickness design of the semi-armor piercing warhead is calculated and analyzed applying the Dimen- sional-Analysis and Similitude-Law as well by the experiment data gained in the cylinder bumping experiment,the rela- tionship curve between the length of the distorted part and its velocity is gained that can be as one of bases while desig- ning the semi-armor piercing warhead.

According to the structure of aircraft carrier and existing anti-ship missile warhead,the structural target with ribbings and experimental half-penetrating warhead were designed with geometer similar principle.

According to the structure of aircraft carrier and existing anti-ship missile warhead, the structural target with ribbings and experimental half-penetrating warhead were designed with geometer similar principle.