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Flight test of a 40 foot nominal diameter disk-gap-band parachute deployed at a Mach number of 3.31 and a dynamic pressure of 10.6 pounds per square foot

机译：40英尺标称直径磁盘 - 带式降落伞的飞行试验，其马力为3.31，动态压力为每平方英尺10.6磅

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摘要

Performance test on disk gap band parachute at supersonic speeds

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作者
Eckstrom, C. V.;
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年度 1970
页码 1-49
总页数 49
原文格式 PDF
正文语种 eng
中图分类工业技术;
关键词
FLIGHT TESTS; PARACHUTES; SUPERSONIC SPEED; AERODYNAMIC DRAG; BRAKES (FOR ARRESTING MOTION); PERFORMANCE TESTS; SUPERSONIC HEAT TRANSFER; UPPER ATMOSPHERE;

机译：飞行测试;降落伞;超音速;空气动力学;制动（争取动作）;性能测试;超音速换热;上层气氛;

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1. Computational Assessment of Facility Wall Loads for Large Parachute Testing in the National Full-Scale Aerodynamics Complex 80- by 120-foot Wind Tunnel [C] . Christopher M. Nykamp, William B. Bartow, Patrick W. Goulding Ⅱ, AIAA aviation forum . 2019

机译：国家全尺寸空气动力学综合大楼80 x 120英尺风洞中大型降落伞测试的设施墙载荷的计算评估
2. Flight Test of a 40 Foot Nominal Diameter Disk-GAP-Band Parachute Deployed at a Mach Number of 3.31 and a Dynamic Pressure of 10.6 Pounds Per Square Foot [R] . Eckstrom, C. V. 1970

机译：40英尺标称直径圆盘-Gap带降落伞的飞行试验，以3.31马赫数和每平方英尺10.6磅的动态压力展开

Flight test of a 40 foot nominal diameter disk-gap-band parachute deployed at a Mach number of 3.31 and a dynamic pressure of 10.6 pounds per square foot

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