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一种新型锥形降落伞的设计 被引量:1

The Design of a New Conical Parachute
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摘要 介绍了两种锥形降落伞的设计。一种伞型使用了零透气量纺织材料,另一种伞型使用了微透气量纺织材料。两种伞型均使阻力系数值达到1.2,从而显著减少了伞衣面积,降低了伞衣重量。 Presents two types of the conical parachute design. One type uses the cloth withlow air permeability for the canopy. The another uses the cloth with zero air permeability.Thecanopy drag coefficient of the two parachutes is increased to 1. 2 and, therefore,the area andthe weight of the parachute canopy are remarkably decreased.
作者 龚文轩
出处 《南京航空航天大学学报》 CAS CSCD 1996年第1期132-136,共5页 Journal of Nanjing University of Aeronautics & Astronautics
关键词 降落伞 伞衣 透气量 阻力系数 parachutes canopy permeability drag coefficient
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参考文献2

  • 1龚文轩,1989年
  • 2龚文轩,1979年

同被引文献9

  • 1熊菁,宋旭民,秦子增.翼伞系统两体相对运动分析[J].航天返回与遥感,2004,25(2):10-16. 被引量:10
  • 2张震宇,明晓.七孔探针的神经网络校准与制造偏差分析[J].实验力学,2005,20(3):473-478. 被引量:3
  • 3HOGUE JEFFREY R, ALLEN WADE R, SMITH ROSS Q. Virtual Reality Entertainment Technology Applied to Military Parachute Simulation Flight Training[C]. AIAA-97-3517, 1997: 83-89.
  • 4JUSTIN BARBER, HAMID JOHARI. Experimental Investigation of Personnel Parachute Designs Using Scale Model Wind Tunnel Testing [C]. 16th AIAA Aerodynamic Decelerator Systems Technology Conference, Boston: MA, AIAA2001-2074, 2001.
  • 5MICHAEl. PAUl. SHANNON, AUGUSTA, GEORGIA. Experimental Analysis of the Pressure Distribution on a 35-foot Personnel Parachute [C]. American Institute of Aeronautics & Astronautics or Published with Permission of Author (s) and/or Author (s)' Sponsoring Organization. AIAA 2001-2008, 2001 : 114- 121.
  • 6DESABRAIS K L, JOHARI H. The Flow in the Near Wake of an Inflating Parachute Canopy [C]. AIAA- 2001-2009, 2001: 122-130.
  • 7DESABRAIS KENNETH J. Velocity Field Measurements in the Near Wake of a Parachute Canopy [R]. Doctor Thesis of Worcester Polytechnic Institute. 2002.
  • 8舒敬荣,王宝贵,韩子鹏,卢春梅.伞—弹系统三体运动分析[J].航空学报,2001,22(6):481-485. 被引量:23
  • 9彭勇,张青斌,程文科,秦子增.降落伞初始充气阶段数值模拟[J].中国空间科学技术,2003,23(3):7-12. 被引量:10

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