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Experiments on Aerothermal Supersonic Fluid-Structure Interaction 气动热超声速流固耦合实验
Pub Date : 2020-10-27 DOI: 10.1007/978-3-030-53847-7_21
Dennis Daub, S. Willems, B. Esser, A. Gülhan
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引用次数: 5
Numerical Analysis of the Turbulent Wake for a Generic Space Launcher with a Dual-Bell Nozzle 通用双钟形喷管空间发射装置湍流尾迹的数值分析
Pub Date : 2020-10-27 DOI: 10.1007/978-3-030-53847-7_10
S. Loosen, M. Meinke, W. Schröder
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引用次数: 0
On the Consideration of Diffusive Fluxes Within High-Pressure Injections 高压注入内扩散通量的考虑
Pub Date : 2020-10-27 DOI: 10.1007/978-3-030-53847-7_12
F. Föll, V. Gerber, C. Munz, B. Weigand, G. Lamanna
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引用次数: 1
Definition and Evaluation of Advanced Rocket Thrust Chamber Demonstrator Concepts 先进火箭推力室验证概念的定义与评价
Pub Date : 2020-10-27 DOI: 10.1007/978-3-030-53847-7_26
Daniel Eiringhaus, H. Riedmann, O. Knab
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引用次数: 0
Heat Transfer in Pulsating Flow and Its Impact on Temperature Distribution and Damping Performance of Acoustic Resonators 脉动流动中的传热及其对声学谐振器温度分布和阻尼性能的影响
Pub Date : 2020-10-27 DOI: 10.1007/978-3-030-53847-7_6
S. V. Buren, W. Polifke
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引用次数: 1
Innovative Cooling for Rocket Combustion Chambers 火箭燃烧室的创新冷却
Pub Date : 2020-10-27 DOI: 10.1007/978-3-030-53847-7_3
Jonas Stefan Peichl, A. Schwab, M. Selzer, H. Böhrk, J. Wolfersdorf
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引用次数: 1
Numerical and Experimental Investigations of Buffet on a Diamond Airfoil Designed for Space Launcher Applications 空间发射用金刚石翼型振动的数值与实验研究
Pub Date : 2019-06-19 DOI: 10.1108/HFF-07-2018-0353
Jéromine Dumon, Y. Bury, N. Gourdain, L. Michel
PurposeThe development of reusable space launchers requires a comprehensive knowledge of transonic flow effects on the launcher structure, such as buffet. Indeed, the mechanical integrity of the launcher can be compromised by shock wave/boundary layer interactions, that induce lateral forces responsible for plunging and pitching moments.Design/methodology/approachThis paper aims to report numerical and experimental investigations on the aerodynamic and aeroelastic behavior of a diamond airfoil, designed for microsatellite-dedicated launchers, with a particular interest for the fluid/structure interaction during buffeting. Experimental investigations based on Schlieren visualizations are conducted in a transonic wind tunnel and are then compared with numerical predictions based on unsteady Reynolds averaged Navier–Stokes and large eddy simulation (LES) approaches. The effect of buffeting on the structure is finally studied by solving the equation of the dynamics.FindingsBuffeting is both experimentally and numerically revealed. Experiments highlight 3D oscillations of the shock wave in the manner of a wind-flapping flag. LES computations identify a lambda-shaped shock wave foot width oscillations, which noticeably impact aerodynamic loads. At last, the experiments highlight the chaotic behavior of the shock wave as it shifts from an oscillatory periodic to an erratic 3D flapping state. Fluid structure computations show that the aerodynamic response of the airfoil tends to damp the structural vibrations and to mitigate the effect of buffeting.Originality/valueWhile buffeting has been extensively studied for classical supercritical profiles, this study focuses on diamond airfoils. Moreover, a fluid structure computation has been conducted to point out the effect of buffeting.
目的研制可重复使用的空间发射装置,需要对发射装置结构的跨声速流效应有全面的了解。事实上,发射装置的机械完整性可能会受到冲击波/边界层相互作用的影响,这种相互作用会产生导致俯冲和俯仰力矩的侧向力。设计/方法/方法本文旨在报告用于微卫星专用发射器的金刚石翼型的气动和气动弹性行为的数值和实验研究,特别关注抖振期间的流体/结构相互作用。在跨声速风洞中进行了基于纹影可视化的实验研究,并与基于非定常Reynolds平均Navier-Stokes方法和大涡模拟(LES)方法的数值预测进行了比较。最后通过求解动力学方程,研究了抖振对结构的影响。发现抖振在实验和数值上都得到了揭示。实验突出了激波的三维振荡,就像一面迎风飘扬的旗帜。LES计算确定了一个λ形激波脚宽振荡,它对气动载荷有明显的影响。最后,实验强调了激波从振荡周期到不稳定三维扑动状态转变时的混沌行为。流体结构计算表明,翼型的气动响应倾向于抑制结构振动和减轻抖振的影响。虽然经典超临界型的抖振已经得到了广泛的研究,但这项研究主要集中在金刚石翼型上。此外,还进行了流体结构计算,以指出抖振的影响。
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引用次数: 1
Boundary Layer Stability with Embedded Rotating Cylindrical Roughness Element 嵌入旋转圆柱粗糙度单元的边界层稳定性
Pub Date : 2018-11-06 DOI: 10.1007/978-3-030-25253-3_27
Yongxiang Wu, U. Rist
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引用次数: 3
Towards CFD-Based Aeroelastic Analysis of NLF Wings 基于cfd的NLF机翼气动弹性分析研究
Pub Date : 2018-11-06 DOI: 10.1007/978-3-030-25253-3_47
Sebastian Helm, Michael Fehrs, J. Nitzsche
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引用次数: 0
Unsteady Wake and Tailplane Loads of the Common Research Model in Low Speed Stall 低速失速下非定常尾流和尾翼载荷的常用研究模型
Pub Date : 2018-11-06 DOI: 10.1007/978-3-030-25253-3_2
A. Waldmann, R. Konrath, T. Lutz, E. Krämer
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引用次数: 2
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Notes on Numerical Fluid Mechanics and Multidisciplinary Design
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