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Aerodynamic characteristics of a modified cone - Conical-frustum entry configuration at Mach 6.0

机译：改进锥体的空气动力学特性 - 马赫数为6.0的锥形截头锥形入口构型

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Aerodynamic characteristics of modified conical lifting reentry vehicle at hypersonic speeds

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作者
Ashby, G. C., Jr.; Staylor, W. F.;
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年度 1968
页码 1-19
总页数 19
原文格式 PDF
正文语种 eng
中图分类工业技术 ;
关键词
AERODYNAMIC CHARACTERISTICS; CONICAL BODIES; HYPERSONIC SPEED; LIFTING REENTRY VEHICLES; COMPUTER PROGRAMS; DECOUPLING; FLIGHT CREWS; MANNED REENTRY; REYNOLDS NUMBER; SPACECRAFT STABILITY; WIND TUNNEL STABILITY TESTS;

机译：空气动力学特征;圆锥体;超速的;提升再生车辆;电脑程序;解耦;飞行的CREWs; mannED REENTRY; REYNOLDs NUmBER;航天器稳定性;风洞稳定性试验;

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专利

1. 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
2. Aerodynamic performance of an over-the-wing propeller configuration at increasing Mach number [J] . L. Mueller, D. Kozulovic, R. Radespiel CEAS Aeronautical Journal . 2014 ,第3期

机译：马赫数增加时机翼螺旋桨配置的空气动力性能
3. The Met Office Unified Model Global Atmosphere 6.0/6.1 and JULES Global Land 6.0/6.1 configurations [J] . Walters David, Boutle Ian, Brooks Malcolm, Geoscientific Model Development Discussions . 2017 ,第4期

机译：大都会办公室统一模型全球大气6.0 / 6.1和JULES全球土地6.0 / 6.1配置
4. Comparison of the Aerodynamic Characteristics of the Eppler-197 and Modified Eppler-197 Airfoil Sections at Mach Number from 0.4 to 0.75 [C] . Tosaporn Soontornpasatch 2018 Third International Conference on Engineering Science and Innovative Technology . 2018

机译：Eppler-197和改进的Eppler-197翼型截面在0.4至0.75马赫数时的气动特性比较
5. Numerical Investigation of Boundary--Layer Transition for Cones at Mach 3.5 and 6.0. [D] . Laible, Andreas C. 2011

机译：圆锥在3.5和6.0马赫处边界层过渡的数值研究。
6. In-depth morphological evaluation of tooth anatomic lengths with root canal configurations using cone beam computed tomography in North American population [O] . Varun KULKARNI, Onurcem DURUEL, Emel Tuğba ATAMAN-DURUEL, 2020

机译：锥形束计算机体层摄影术在北美人群中对根管构型的牙齿解剖长度进行深度形态学评估
7. Aerodynamic characteristics of a wedge and cone at hypersonic mach numbers. [O] . De Lauer Richard D. 1950

机译：高超声速马赫数下楔形和圆锥形的空气动力学特性。
8. Aerodynamic Characteristics of a Modified Cone - Conical-Frustum Entry Configuration at Mach 6.0 [R] . Ashby, G. C., Staylor, W. F. 1968

机译：改进的圆锥 - 锥形入口结构在6.0马赫处的气动特性

Aerodynamic characteristics of a modified cone - Conical-frustum entry configuration at Mach 6.0

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