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Experimental investigation of the zero-lift drag of a fin-stabilized body of fineness ratio 10 at Mach numbers between 0.6 and 10

机译：在马赫数为0.6和10之间的细度稳定体10的零升力阻力的实验研究

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James, Carlton S; Carros, Robert J;
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年度 1953
页码 1-37
总页数 37
原文格式 PDF
正文语种 eng
中图分类工业技术;
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1. 大长径比带翼刚体的零升阻力系数和升力系数与马赫数的相关性（英文） [J] . 董素荣测试科学与仪器：英文版 . 2015,第003期
2. Experimental Evaluation of a High Fineness Ratio Body with Drag Brakes [J] . Corey J. Florendo, Thomas R. Yechout, Stefan Siegel, Journal of Spacecraft and Rockets . 2007,第3期

机译：高阻力比高阻体车身的实验评估
3. Experimental investigation of drag reduction by forward facing high speed gas jet for a large angle blunt cone at Mach 8 [J] . Balla Venukumar, K. P. J. Reddy Sadhana . 2007,第1a2期

机译：8马赫大角度钝锥前向高速气体射流减阻实验研究。
4. Experimental investigation of drag reduction by forward facing high speed gas jet for a large angle blunt cone at Mach 8 [J] . BALLA VENUKUMAR, K. P. J. REDDY Sadhana: Academy Proceedings in Engineering Science . 2007,第1a2期

机译：8马赫大角度钝锥前向高速气体射流减阻实验研究。
5. Experimental and Computational Investigation of Drag Reduction by Electric-Arc Airspikes at Mach 10 [C] . C. S. Hartley, T. W. Portwood, M. V. Filippelli, International Symposium on Beamed Energy Propulsion . 2005

机译：Mach 10电弧空气阻力减阻试验和计算调查
6. Experimental pressure and heat transfer investigation over a "directed-energy air spike" inlet at flow mach numbers of 10 to 20, stagnation temperature of 1000 K, and arc powers up to 127 KW. [D] . Toro, Paulo Gilberto de Paula. 1998

机译：在流量为10至20的马赫数，停滞温度为1000 K，电弧功率高达127 KW的“定向能空气尖峰”入口上进行实验压力和传热研究。
7. Infection with Mycobacterium avium induces production of interleukin-10 (IL-10) and administration of anti-IL-10 antibody is associated with enhanced resistance to infection in mice. [O] . L E Bermudez, J Champsi 1993

机译：鸟分枝杆菌感染会诱导白介素10（IL-10）的产生抗IL-10抗体的给药与小鼠抗感染能力增强相关。
8. An experimental investigation of an airframe integrated three-dimensional scramjet engine at a Mach 10 flight condition [O] . Doherty Luke James 2014

机译：在10马赫飞行条件下机体集成三维超燃冲压发动机的实验研究

Experimental investigation of the zero-lift drag of a fin-stabilized body of fineness ratio 10 at Mach numbers between 0.6 and 10

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