弹翼展开装置研究

Study on Launching Installment of Missile Wing

介绍了弹翼展开装置的计算模型、载荷条件、研制方案、测试电路、试验结果等,在地面模拟确定弹翼展开过程中所需的气动力参数,从而优化了作动筒参数,保证了弹翼的顺利展开。

For missile wing,introduce its computation model,load conditions,development plan,test circuit,test results etc.,simulate and acquire aerodynamic coefficients while launching installment of missile wing in ground,finally opti- mize actuator coefficients and ensure launching missile wing.