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Static stability and axial force characteristics of a 1.32 percent scale model of the Saturn IB/Apollo, its components, and the Saturn IB/Apollo/Minuteman launch vehicle, determined by wind tunnel test

机译：通过风洞试验确定的土星IB /阿波罗及其部件和土星IB /阿波罗/民兵运载火箭的1.32％比例模型的静态稳定性和轴力特性

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Wind tunnel stability tests of scale model Saturn IB/Apollo, and Saturn IB/Apollo/ Minuteman launch vehicle

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作者
Chianese, F.;
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作者单位

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年度 1965
页码 1-91
总页数 91
原文格式 PDF
正文语种 eng
中图分类工业技术;
关键词
APOLLO SPACECRAFT; MACH NUMBER; MINUTEMAN ICBM; REYNOLDS NUMBER; SATURN LAUNCH VEHICLES; SATURN 1B LAUNCH VEHICLES; SCALE MODELS; STATIC STABILITY; WIND TUNNEL STABILITY TESTS; WIND TUNNEL TESTS; APOLLO SPACECRAFT; MINUTEMAN ICBM; SATURN IB LAUNCH VEHICLE; WIND TUNNEL STABILITY TEST;

机译：apOLLO spaCECRaFT;马赫数; mINUTEmaN洲际弹道导弹; REYNOLDs NUmBER; saTURN推出车辆; saTURN 1B发射车辆;尺度模型;静态稳定性;风洞稳定性试验;风洞隧道测试; apOLLO spaCECRaFT; mINUTEmaN洲际弹道导弹; saTURN IB LaUNCH车辆;风洞稳定性试验;

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1. Study of the Wind Tunnel Effect on the Drag Coefficient (C_D) of a Scaled Static Vehicle Model Compared to a Full Scale Computational Fluid Dynamic Model [J] . Sanwar A. Sunny Asian Journal of Scientific Research . 2011,第3期

机译：风洞对比例静态车辆模型与全比例计算流体动力学模型的阻力系数（C _{D ）的影响研究}
2. Design, modelling and analysis of a six component force balance for hypervelocity wind tunnel testing [J] . A.L. Smith, D.J. Mee, W.J.T. Daniel Computers & Structures . 2001,第11期

机译：超高速风洞测试中六分量力平衡的设计，建模和分析
3. WIND TUNNEL MODEL ELASTIC SCALING FOR SIMULATIONS OF LAUNCH VEHICLES SUBJECTED TO GROUND WIND EXCITATION [C] . Jim Gillman Proceedings of the Twenty-Fourth International Symposium on Space Technology and Science: Selected Papers . 2004

机译：风洞激励下的车辆动力学模拟风洞模型
4. 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

机译：MACH 0.7 MACH 0.7埃斯利翁发射车气动特性的风洞试验及数值分析

Static stability and axial force characteristics of a 1.32 percent scale model of the Saturn IB/Apollo, its components, and the Saturn IB/Apollo/Minuteman launch vehicle, determined by wind tunnel test

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