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计算了某高超音速火箭的气动特性 ,并用风洞试验数据进行比较 ,验证了计算方法是可靠的。在此基础上 ,用该方法计算了高超音速导弹各种常见外形的气动特性 ,形成数据库 ,便于今后在工程上应用
The aerodynamic characteristics of a hypersonic rocket are calculated and compared with wind tunnel test data to verify that the calculation method is reliable. On this basis, the aerodynamic characteristics of various common hypersonic missile hypersonic missiles are calculated by this method to form a database for future application in engineering