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Explorator heat-transfer measurements at Mach 10 on a 7.5 deg total-angle cone downstream of a region of air and helium transpiration cooling

机译：在空气和氦气蒸发冷却区域下游的7.5度全角锥上以10马赫进行探测器传热测量

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摘要

Heat transfer measurements at Mach 10 on total angle cone downstream of air and helium transpiration cooling region

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Dunavant, J. C.; Everhart, P. E.;
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年度 1969
页码 1-32
总页数 32
原文格式 PDF
正文语种 eng
中图分类工业技术;
关键词
AERODYNAMIC HEATING; HEAT TRANSFER; SWEAT COOLING; THERMODYNAMIC PROPERTIES; AIR; HELIUM; MACH NUMBER; POROUS BOUNDARY LAYER CONTROL; SURFACE REACTIONS; TRANSITION FLOW; TURBULENT FLOW;

机译：空气动力加热;传播热量; sWEaT COOLING;热力学性质;空气;氦;马赫数;多孔边界层控制;表面反应;过渡流动;湍流;

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1. Deformation behavior of Zr_(55.9)Cu_(18.6)Ta_8Al_(7.5)Ni_(10) bulk metallic glass matrix composite in the supercooled liquid region [J] . K.C. Chan, Q. Chen, L. Liu Intermetallics . 2007,第4期

机译：Zr_（55.9）Cu_（18.6）Ta_8Al_（7.5）Ni_（10）块状金属玻璃基复合材料在过冷液体区的变形行为
2. Numerical Study of Flow Angles and Mach Number Measurement Using the Surface Pressure of a Supersonic Aircraft with Nose Cone [J] . Katsuyoshi Fukiba, Nobuyuki Tsuboi, Hiroaki Kobayashi Transactions of the Japan society for aeronautical and space sciences . 2012,第2期

机译：超音速机鼻锥面流角和马赫数测量的数值研究。
3. Air Density Measurements in a Mach 10 Wake Using Iodine Cordes Bands [J] . R. Jeffrey Balla, Joel L. Everhart AIAA Journal . 2012,第6期

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4. SURFACE PRESSURE MEASUREMENTS ON A FLAT PLATE AND A 7DEG HALF-CONE AT MACH 6 [C] . Davide Masutti, Erkan Gunaydinoglu, Olivier Chazot Proceedings of the 7th European symposium on aerothermodynamics. . 2011

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5. Hypersonic boundary-layer transition measurements at Mach 10 on a large seven-degree cone at angle of attack [D] . Moraru, Ciprian G. 2015

机译：在大七度锥面的迎角处以10马赫的高超声速边界层跃迁测量
6. Deformation behavior of Zr55.9Cu18.6Ta8Al7.5Ni10 bulk metallic glass matrix composite in the supercooled liquid region [O] . Chan KC, Chen Q, Liu L 2007

机译：Zr55.9Cu18.6Ta8Al7.5Ni10大块金属玻璃基复合材料在过冷液体区的变形行为
7. Explorator Heat-Transfer Measurements at Mach 10 on a 7.5 Deg Total-Angle Cone Downstream of a Region of Air and Helium Transpiration Cooling [R] . Dunavant, J. C., Everhart, P. E. 1969

机译：在空气和氦气蒸发冷却区域下游7.5度全角锥上以10马赫进行探测器传热测量

Explorator heat-transfer measurements at Mach 10 on a 7.5 deg total-angle cone downstream of a region of air and helium transpiration cooling

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