LOAD ANALYSIS SYSTEM AND LOAD ANALYSIS METHOD TO DESIGN THE INTERNAL WEAPON BAY OF FIFTH GENERATION AIRCRAFT

摘要

PURPOSE: A load analysis system and a load analysis method for designing the internal weapon bay (IWB) of fifth generation aircraft are provided to calculate a load necessary for the IWB, the system for carrying arms equipment, the system for launching and releasing the arms equipment, and the opening and shutting of the cover of the IWB. CONSTITUTION: A base data extraction module (100) sets up the predetermined demanding and designing standards and extracts base data for IWB design. A data generation module (200) generates weight data based on the base data. A calculation module (300) calculates a load for IWB design using the weight data. A result output module (400) outputs a load value for IWB design.