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Supersonic aerodynamic characteristics of a Saturn IB launch vehicle model with third-stage modifications

机译：具有第三阶段修改的土星IB运载火箭模型的超音速空气动力学特性

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Wind tunnel test of Saturn IB launch vehicle to determine effects of change in third stage cone angle and Apollo spacecraft escape tower on aerodynamic characteristics in pitch

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作者
Fournier, R. H.;
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年度 1966
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; APOLLO SPACECRAFT; LAUNCH VEHICLES; SATURN LAUNCH VEHICLES; SATURN 1B LAUNCH VEHICLES; TOWERS; WIND TUNNEL TESTS; AERODYNAMIC CHARACTERISTICS; APOLLO SPACECRAFT; SATURN IB LAUNCH VEHICLE;

机译：空气动力学特征; apOLLO spaCECRaFT;发射车辆; saTURN推出车辆; saTURN 1B发射车辆;塔;风洞隧道测试;空气动力学特征; apOLLO spaCECRaFT; saTURN IB LaUNCH车辆;

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1. Numerical Modeling of the Effect of Geometric Asymmetry on the Damping Aerodynamic Characteristics of Supersonic Sectional Flight Vehicles [J] . A. V. Antonets Fluid Dynamics . 2006,第3期

机译：几何不对称对超音速分段飞行器阻尼空气动力学特性影响的数值模拟
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

机译：装有超音速呼吸飞行器的运载火箭的计算和实验空气动力学特性
3. Experimental study of aerodynamic characteristics of a reentry vehicle on a setup with free oscillations at supersonic velocities [J] . Adamov N. P., Kharitonov A. M., Chasovnikov E. A., Thermophysics and Aeromechanics . 2016,第6期

机译：超音速自由振荡条件下再入飞行器空气动力学特性的实验研究
4. Ground Vehicle Optimization regarding Aesthetic Completeness and Aerodynamic Characteristics by modification of Vehicle Modeling Function and Conceptual Design Process [C] . Doe Young Hur, Dongho Lee AIAA aerospace sciences meeting including the new horizons forum and aerospace exposition . 2013

机译：通过修改车辆建模功能和概念设计过程优化地面车辆的美学完整性和空气动力学特性
5. Aerodynamic flight control to provide flight control augmentation for aft-cg future launch vehicles. [D] . Barret, Christian. 1996

机译：空气动力学飞行控制，为后cg未来发射飞行器提供飞行控制增强。
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. 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
8. Supersonic Aerodynamic Characteristics of a Saturn Ib Launch Vehicle Model with Third-Stage Modifications [R] . Fournier, R. H. 1966

机译：具有第三阶段修正的土星Ib运载火箭模型的超音速气动特性

Supersonic aerodynamic characteristics of a Saturn IB launch vehicle model with third-stage modifications

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