利用风洞试验研究冲压翼伞的升阻特性  

STUDY ON LIFT DRAG CHARACTERISTIC OF RAM AIR PARACHUTE IN WIND TUNNEL

作　　者：贺卫亮[1] 

机构地区：[1]北京空间机电研究所

出　　处：《航空学报》1999年第S1期76-78,共3页Acta Aeronautica et Astronautica Sinica

摘　　要：冲压翼伞的风洞试验是研制冲压翼伞过程中的一项重要内容。介绍了投物用冲压翼伞风洞试验的特点及发展，着重讨论了这类冲压翼伞的升阻特性，通过理论计算与试验结果的比较，分析了柔翼与刚性翼之间的差异，得出了升阻比最佳点，同时，还分析了冲压翼伞各部分阻力的构成情况，提出了减少阻力的主要措施。Wind tunnel test is an important phase in the development of ram air parachutes. In this paper, the emphasis is put on the lift drag characteristic. By comparing the theoretical analysis with test result,the difference between flexible wing and rigid wing is introduced, and the optimum point of lift drag ratio is obtained. Meanwhile, the constitution of drag forces in the ram air parachute is also analysed, and the method to reduce the drag force is put forward.

关 键 词：冲压翼伞 风洞试验 升阻特性 

分 类 号：V211.59[航空宇航科学与技术—航空宇航推进理论与工程]