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Aerodynamic Characteristics of Several Proposed Versions of the Saturn V Launch Vehicle at Mach Numbers 1.57 to 4.65

机译：土星V运载火箭的几种拟议版本的气动特性，马赫数为1.57至4.65

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作者
Fuller, D. E.; Fournier, R. H.;
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年度 1964
页码 1-3
总页数 3
原文格式 PDF
正文语种 eng
中图分类工业技术;
关键词
Launch vehicles ; Aerodynamic characteristics ; Mach number;

机译：运载火箭;空气动力学特性;马赫数;

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2. Computational and Experimental Aerodynamic Characteristics of Launch Vehicle Housing a Hypersonic Air-breathing Vehicle [J] . S Sriram, G Balu Journal of the Institution of Engineers (Inida) . 2007,第May期

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3. Aerodynamic characteristics of a novel catapult launched morphing tandem-wing unmanned aerial vehicle: [J] . Liang Gao, Changle Li, Hongzhe Jin, Advances in Mechanical Engineering . 2017,第2期

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4. Ascent flight aerodynamic characteristics of the national launch system 1 1/2-stage launch vehicle: nls-2 [C] . A. Springer, D. Pokora AIAA 32nd Aerospace Sciences Meeting Exhibit January 10-13, 1994/Reno, NV . -1

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5. Aerodynamic flight control to provide flight control augmentation for aft-cg future launch vehicles. [D] . Barret, Christian. 1996

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7. Wind Tunnel Tests and Numerical Analyses on Aerodynamic Characteristics of Epsilon Launch Vehicle at Mach 0.7 [O] . Keiichi KITAMURA, Kazuto KUZUU, Tomoko IRIKADO, 2011

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Aerodynamic Characteristics of Several Proposed Versions of the Saturn V Launch Vehicle at Mach Numbers 1.57 to 4.65

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