论文部分内容阅读
飞机干扰条件下的非圆截面布撒器的气动力计算是新型航空布撒器研制中的关键技术之一。对伍德沃德提出的面元法加以改进,用改进的面元法计算了在飞机干扰下某型非圆截面布撒器的气动力,与无干扰条件下的计算结果进行了比较,并作了简要分析。
The aerodynamic calculation of a non-circular cross-section dispenser under aircraft disturbance is one of the key technologies in the development of a new type of aerosol dispenser. The improved Woodward method is proposed to improve the surface element method. The aerodynamic force of some non-circular cross-section scatterer under the aircraft disturbance is calculated by the improved method of the surface element. Compared with the non-interference calculation, A brief analysis.