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Transonic-wind-tunnel investigation of the effects of lip bluntness and shape on the drag and pressure recovery of a normal-shock nose inlet in a body of revolution

机译：跨声 - 风洞研究唇形钝头和形状对旋转体中正常冲击鼻入口的阻力和压力恢复的影响

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Olstad, Walter B;
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年度 1956
页码 1-46
总页数 46
原文格式 PDF
正文语种 eng
中图分类工业技术;
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1. Aerodisk effects on drag reduction for hypersonic blunt body with an ellipsoid nose [J] . Zhong Kang, Yan Chao, Chen Shu-sheng, Aerospace science and technology . 2019,第MARa期

机译：Aerodisk对椭圆形鼻子高超声速钝体减阻的影响
2. Drag Reduction and Aerodynamic Shape Optimization for Spike-Tipped Supersonic Blunt Nose [J] . Xue Yuan, Wang Liang, Fu Song Journal of Spacecraft and Rockets . 2018,第3期

机译：尖峰超音速钝鼻的减阻和空气动力学形状优化
3. Drag Reduction for Spike Attached to Blunt-Nosed Body at Mach 6 [J] . R Kalimuthu, Rakhab C. Mehta, E Rathakrishnan Journal of Spacecraft and Rockets . 2010,第1期

机译：减少减震力，以使附着在马赫数为6的钝头物体上的尖刺
4. Pressures and Drag Characteristics of Bodies of Revolution at Near Sonic Speeds Including the Effects of Viscosity and Wind Tunnel Walls [C] . B. Kulfan, J. Bussoletti, C. Hilmes AIAA Aerospace Sciences Meeting and Exhibit . 2007

机译：接近声速时旋转体的压力和阻力特性，包括粘度和风洞壁的影响
5. Effects of nose bluntness and shock-shock interactions on blunt bodies in viscous hypersonic flows. [D] . Singh, Dal Jeet. 1989

机译：鼻子过钝和电击-相互作用对粘性高超声速流动中钝体的影响。
6. Wind-Tunnel Investigations of Blunt-Body Drag Reduction Using Forebody Surface Roughness [O] . Curry, Robert E., Whitmore, Stephen A., Sprague, Stephanie, 2001

机译：利用前体表面粗糙度减少钝体阻力的风洞研究

Transonic-wind-tunnel investigation of the effects of lip bluntness and shape on the drag and pressure recovery of a normal-shock nose inlet in a body of revolution

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