首页|不同操纵方式对十字伞滑翔性能的影响研究

不同操纵方式对十字伞滑翔性能的影响研究

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为拓展十字伞的应用场景,提高十字伞的滑翔能力,采用数值模拟手段研究不同操纵方式对十字伞滑翔性能的影响.方法一是从伞绳收口的角度,通过对十字伞的伞绳进行不同程度的收口形成角空气喷口,达到操纵十字伞的目的;方法二是从改变伞衣几何透气性的角度,通过加装排气扰流板并使其偏转不同的角度,达到操纵十字伞的目的.数值结果表明:角空气喷口中的伞绳收口程度对十字伞俯仰角的变化影响较为显著,十字伞俯仰角最大可达 2°;排气扰流板的偏转角度则对十字伞侧向力的影响较为显著,在偏转角达到 30°时,侧向力达到最大,为47.3 N.2 种操纵方式均能够使十字伞具备一定的滑翔能力.
Effect of Different Steering Approaches on Gliding Performance of Cruciform Parachute
In order to expand the application of cruciform parachute and improve the gliding per-formance of cruciform parachutes,the effect of different steering approaches on the gliding perform-ance of cruciform parachute was studied numerically.One steering method was reefing the cables to some extent to form the air-venting corner such that cruciform parachute could be steered.The other method was changing the geometrical porosity of the canopy,i.e.,by installing a bleed air spoiler on the canopy surface and changing the deflection angle to steer the parachute.The simulation re-sults showed that the reefing extent of the cables had a significant impact on the pitch angle of the parachute,which could reach 2°at most.While the deflection angle of the bleed air spoiler had a significant impact on the lateral force of the parachute,when the deflection angle reached 30°,the lateral force reached its maximum at 47.3N.It is demonstrated that both steering approaches are ef-fective for the gliding performance of the cruciform parachute.

cruciform parachutereefingbleed air spoilergliding performancefluid-structure in-teraction

黄云尧、武士轻、张扬

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南京航空航天大学航天学院,南京 210016

北京空间机电研究所,北京 100094

中国航天科技集团有限公司航天进入、减速与着陆技术实验室,北京 100094

十字伞 伞绳收口 排气扰流板 滑翔性能 流固耦合

航天科技集团航天进入减速与着陆技术实验室开放基金

EDL19092128

2024

载人航天
中国载人航天工程办公室

载人航天

CSTPCD北大核心
影响因子:0.411
ISSN:1674-5825
年,卷(期):2024.30(1)
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