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Effects of Cone Angle, Base Flare Angle, and Corner Radius on Mach 3.0 Aerodynamic Characteristics of Large-Angle Cones

机译：锥角，基角和角半径对大角锥mach 3.0气动特性的影响

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作者
Deveikis, W. D.; Sawyer, J. W.;
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年度 1969
页码 1-4
总页数 4
原文格式 PDF
正文语种 eng
中图分类工业技术;
关键词
Aerodynamic characteristics ; Angles (geometry) ; Conical bodies ; Mach number ; Wind tunnel models ; Angle of attack ; Dimensions ; Wind tunnel stability tests;

机译：空气动力学特性;角度（几何）;锥形体;马赫数;风洞模型;迎角;尺寸;风洞稳定性试验;

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1. Flow Fields of a Large-Angle, Spiked Blunt Cone at Hypersonic Mach Numbers [J] . Jagadeesh GOPALAN, Viren MENEZES, K.P. Jagannatha REDDY, Transactions of the Japan society for aeronautical and space sciences . 2005,第160期

机译：高超声速马赫数的大角度尖刺钝锥的流场
2. AN APPRAISAL OF SWIRL ATOMIZER INVISCID FLOW ANALYSIS, PART 2: INVISCID SPRAY CONE ANGLE ANALYSIS AND COMPARISON OF INVISCID METHODS WITH EXPERIMENTAL RESULTS FOR DISCHARGE COEFFICIENT, AIR CORE RADIUS, AND SPRAY CONE ANGLE [J] . John Joss Chinn Atomization and Sprays: Journal of the International Institutes for Liquid Atomization and Spray Systems . 2009,第3期

机译：旋流式原子流分析方法的评估，第2部分：喷嘴喷雾锥角分析以及喷嘴方法与排放系数，空气芯半径和喷雾锥角的实验结果的比较
3. EFFECT OF FLARE ANGLE AND NATURAL VENTILATION ON THE AERODYNAMIC CHARACTERISTICS OF A TYPICAL RE-ENTRY BODY AT SUBSONIC AND TRANSONIC MACH NUMBERS [J] . G.K. Suryanarayana Journal of Aerospace Sciences and Technologies . 2011,第4期

机译：喇叭口角和自然通风对次音速和超音速马赫数典型再入体气动特性的影响
4. Aerodynamic Drag Reduction Using Aerospikes for Large Angle Blunt Cone Flying at Hypersonic Mach Number [C] . V. Menezes, S. Saravanan, G. Jagadeesh, AIAA Fluid Dynamics Conference and Exhibit . 2002

机译：使用气钉降低空气阻力，以高超声速马赫数飞行大角度钝锥
5. Parametric Study of a 7° Half-angle Cone with Highly-swept Fins at Mach 6 [D] . Turbeville, Franklin Drew. 2018

机译：在马赫6中具有高扫翅片的7°半角锥的参数研究
6. Accurate T1 Mapping of Short T2 Tissues Using a Three-Dimensional Ultrashort Echo Time Cones Actual Flip Angle Imaging Variable Repetition Time (3D UTE-Cones AFI-VTR) Method [O] . Ya-Jun Ma, Xing Lu, Michael Carl, -1

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7. Effect of flare angle and natural ventilation on the aerodynamic characteristics of a typical re-entry body at subsonic and transonic mach numbers [O] . Suryanarayana GK 2011

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8. Effects of cone angle, base flare angle, and corner radius on Mach 3.0 aerodynamic characteristics of large-angle cones [R] . Deveikis, W. D., Sawyer, J. W. 1969

机译：锥角，基座喇叭口角和转角半径对大角度锥体mach 3.0空气动力学特性的影响

Effects of Cone Angle, Base Flare Angle, and Corner Radius on Mach 3.0 Aerodynamic Characteristics of Large-Angle Cones

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