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Wind tunnel investigation of inflation of disk-gap-band and modified ringsail parachutes at dynamic pressures between 0.24 and 7.07 pounds per square foot

机译：在动态压力在0.24和7.07磅/平方英尺之间的磁隙带和改进的环形降落伞的充气风洞研究

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Wind tunnel tests of inflatable disk-gap-band and modified ringsail parachutes at low dynamic pressure

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作者
Whitlock, C. H.;
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年度 1969
页码 1-19
总页数 19
原文格式 PDF
正文语种 eng
中图分类工业技术;
关键词
DYNAMIC RESPONSE; INFLATABLE STRUCTURES; PARACHUTES; PERFORMANCE TESTS; AERODYNAMIC CONFIGURATIONS; DISKS (SHAPES); LOW PRESSURE; POROUS MATERIALS; RING STRUCTURES; WIND TUNNELS;

机译：动态响应;可充气结构;降落伞;性能测试;空气动力学配置;磁盘（形状）;低压;多孔材料;环结构;风洞;
入库时间 2022-08-29 11:14:40

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2. Upwind sail aerodynamics: A RANS numerical investigation validated with wind tunnel pressure measurements [J] . I.M. Viola, P. Bot, M. Riotte International Journal of Heat and Fluid Flow . 2013,第feba期

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3. Wind tunnel and computational fluid dynamics study of wind conditions in an urban square [J] . Balczo Marton, Tomor Andras Idojaras . 2016,第2期

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4. Wind Tunnel Test of Subscale Ringsail and Disk-Gap-Band Parachutes [C] . Carlie H. Zumwalt, Juan R. Cruz, Donald F. Keller, AIAA applied aerodynamics conference;AIAA aviation forum . 2016

机译：次尺度环帆和磁盘间隙带降落伞的风洞测试
5. Initial investigations of transonic turbine aerodynamics using the Carleton University High-Speed Wind Tunnel. [D] . Jeffries, Michael Scott. 2001

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6. Estimates for the Aerodynamic Coefficients of Ringsail and Disk-Gap-Band Parachutes Operating on Mars [O] . Juan R. Cruz, Miranda L. Snyder 2017

机译：在火星上运行的ringsail和磁盘间隙带降落伞空气动力学系数的估计
7. Wind Tunnel Investigation of Inflation of Disk-GAP-Band and Modified Ringsail Parachutes at Dynamic Pressures Between 0.24 and 7.07 Pounds Per Square Foot [R] . Whitlock, C. H. 1969

机译：盘式Gap带和改进型Ringsail降落伞在动态压力下每平方英尺0.24和7.07磅之间的通风风洞调查

Wind tunnel investigation of inflation of disk-gap-band and modified ringsail parachutes at dynamic pressures between 0.24 and 7.07 pounds per square foot

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