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Aerodynamic characteristics of the HL-10 manned lifting entry vehicle at Mach 0.95 to 1.20

机译：HL-10有人驾驶起重车的空气动力学特性为0.95至1.20马赫

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作者
Harris, C. D.;
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年度 1968
页码 1-32
总页数 32
原文格式 PDF
正文语种 eng
中图分类工业技术;
关键词
AERODYNAMIC CHARACTERISTICS; LIFTING REENTRY VEHICLES; MANNED SPACE FLIGHT; LONGITUDINAL STABILITY; WIND TUNNEL STABILITY TESTS;

机译：空气动力学特征;提升再生车辆;曼联空间飞行;纵向稳定性;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 design of a re-entry capsule for high-speed manned re-entry [J] . Chen Bingyan, Zhan Huiling, Zhou Weijiang Acta astronautica . 2015,第janaafeba期

机译：高速载人再入舱的再入舱气动设计
3. Integrated analysis of aerodynamic/stealth characteristics of blended-wing-body lifting vehicle [J] . Ye Tao, Jianquan Ge, Qiangqiang Xu, MATEC Web of Conferences . 2017,第1期

机译：混纺机翼体升降车的空气动力学/隐形特性综合分析
4. CFD-BASED AERODYNAMIC SHAPE OPTIMIZATION OF A MANNED RE-ENTRY VEHICLE [C] . M. M. Entezari, M. Mohammadi-Amin Congress of the International Council of the Aeronautical Sciences;International Council of the Aeronautical Sciences . 2014

机译：基于CFD的再入车辆气动形状优化
5. Design issues associated with the use of flaps for atmospheric entry aerodynamic trim control on a manned lunar return capsule. [D] . Andersen, Benjamin Marc. 2007

机译：与将襟翼用于载人登月舱上的大气进入空气动力学内饰控制相关的设计问题。
6. Aerodynamic Characteristics of the Ventilated Design for Flapping Wing Micro Air Vehicle [O] . G. Q. Zhang, S. C. M. Yu -1

机译：拍打翼微型飞机通风设计的空气动力学特性
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

机译：在亚音速和跨音速马赫数下，耀斑角度和自然通风对典型再入物体空气动力学特性的影响
8. Aerodynamic characteristics of the HL-10 manned lifting entry vehicle at a Mach number of 10.5 [R] . Ladson, C. L. 1968

机译：具有10.5马赫数的HL-10有人驾驶起重车的空气动力学特性

Aerodynamic characteristics of the HL-10 manned lifting entry vehicle at Mach 0.95 to 1.20

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