Research on Missile Jet-Airplane Interaction by an Experimental Method

摘要

Based on the local dynamic similarity theory, the experimental apparatus of modeling missile jet-airplane interaction have been set up. The pressure and temperature test systems have been improved. In order to achieve high accuracy of test results, the heating influence of pressure and temperature has been diminished. Several new structures for controlling the strength of shock wave that acts on airplane body and is caused by missile jet have been designed and tested. The flow mechanism of missile jet-airplane interaction has been well understood and some technical measurements for controlling shock wave have been explored.