SYSTEM AND METHOD FOR NUMERICAL SIMULATION OF AIRCRAFT FLOW FIELD

摘要

The present invention on one hand relates to a numerical computation based simulation system for simulating an aircraft flow field. The numerical computation based simulation system may comprise: a computer readable storage medium, which comprises a data receiving module capable of receiving data, a grid processing module capable of performing aircraft flow field grid processing on the received data to generate a processing result, a computational solving module capable of solving and computing a governing equation according to the grid processing result to generate a computational result for an aircraft flow field, and a result analysis module capable of further analyzing the generated computational result for the aircraft flow field to generate an analysis resu and a processor capable of executing executable modules stored in the computer readable storage medium. The present invention on the other hand relates to a numerical computation based simulation method for simulating an aircraft flow field, comprising receiving data, performing aircraft flow field grid processing according to the received data, solving and computing a governing equation to obtain a computational result for a flow field after the processing, and further analyzing the extracted computational result for the aircraft flow field.