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Effect of body nose blunting, control planform area, and leading-edge bluntness on aerodynamic control of a 5 deg semivertex cone at Mach number 6.9

机译：体鼻钝化，控制平面区域和前缘钝性对马赫数为6.9的5度半圆锥体的气动控制的影响

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摘要

Effect of body nose blunting, control planform area, and leading edge bluntness on aerodynamic control of semivertex cone at hypersonic speed

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作者
Penland, J. A.;
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年度 1966
页码 1-68
总页数 68
原文格式 PDF
正文语种 eng
中图分类工业技术;
关键词
AERODYNAMICS; ATTITUDE CONTROL; BLUNT BODIES; CONTROL SURFACES; DYNAMIC CONTROL; HYPERSONIC SPEED; LEADING EDGES; NOSE CONES; PLANFORMS; BLUNT BODY; CONTROL SURFACE; DYNAMIC CONTROL; HYPERSONIC SPEED; LEADING EDGE;

机译：空气动力学;态度控制; BLUNT BODIEs;控制表面;动态控制;超速的;领先的边缘;鼻子锥;平面形状; BLUNT BODY;控制面;动态控制;超速的;领先的边缘;

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1. Nose micro-blowing for asymmetric vortices control on blunt-nose slender body at high angle of attack [J] . Lei Wang, Yankui Wang, Zhongyang Qi 力学快报(英文版) . 2017,第006期

机译：鼻子微吹可在高攻角下控制钝鼻细长体的不对称涡流
2. Leading-edge bluntness effects on aerodynamic heating and drag of power law body in low-density hypersonic flow [J] . Santos W. F. N. Journal of the Brazilian Society of Mechanical Sciences and Engineering . 2005,第3期

机译：低密度高超音速流动中前沿钝性对动力定律气动动力和阻力的影响
3. Leading-edge bluntness effects on aerodynamic heating and drag of power law body in low-density hypersonic flow [J] . Santos W. F. N. Journal of the Brazilian Society of Mechanical Sciences and Engineering . 2005,第3期

机译：低密度高超音速流动中前沿钝性对动力定律气动动力和阻力的影响
4. Nonlinear stability of straight cones with sharp and blunt noses at Mach 6 [C] . Arham Amin Khan, Armani Batista, Joseph Kuehl AIAA SciTech forum and exposition . 2020

机译：鼻尖尖钝的直锥的非线性稳定性为6马赫
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. Impact on survival of whole-body computed tomography before emergency bleeding control in patients with severe blunt trauma [O] . Daiki Wada, Yasushi Nakamori, Kazuma Yamakawa, 2013

机译：严重钝性创伤患者紧急控制出血前对全身计算机断层扫描的生存的影响
7. Leading-edge bluntness effects on aerodynamic heating and drag of power law body in low-density hypersonic flow [O] . W. F. N. Santos 2005

机译：低密度高超音速流动中前沿钝性对动力定律和空气动力加热和阻力的影响
8. Effect of Body Nose Blunting, Control Planform Area, and Leading-Edge Bluntness on Aerodynamic Control of a 5 Deg Semivertex Cone at Mach Number 6.9 [R] . Penland, J. A. 1966

机译：体鼻钝化，控制平面区域和前缘钝角对马赫数为6.9的5度半圆锥体气动控制的影响

Effect of body nose blunting, control planform area, and leading-edge bluntness on aerodynamic control of a 5 deg semivertex cone at Mach number 6.9

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