Application of Broadband Receptivity Data to the Amplitude Method for Transition Prediction

IF 1.3 4区 工程技术 Q2 ENGINEERING, AEROSPACE
Simon He, X. Zhong
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引用次数: 0

Abstract

Conventional hypersonic transition prediction relies upon the highly empirical [Formula: see text] method, which is predicated on theoretical approximations of relative disturbance growth. This does not account for the receptivity mechanism and the high degree of variability present in experimental wind-tunnel conditions, which itself leads to high degrees of variability in transition [Formula: see text] factors. The amplitude method, which better approximates the broadband nature of boundary-layer disturbances, was previously proposed to account for the effects of receptivity. In this study, high-fidelity simulated second-mode receptivity data for two blunt cones at Mach 10 to broadband disturbances are applied to an iterative approximation of the amplitude method tuned for second-mode dominated flows. The studied geometries consist of 9.525- and 5.080-mm-nose-radius 7 deg half-angle straight cones based on experimental cases from Arnold Engineering Development Center’s wind tunnel 9. Amplitude method predictions show improvement over the accuracy of [Formula: see text] estimates using standard threshold [Formula: see text] factors. In particular, the less blunt 5.080 mm cone demonstrates the best agreement due to its stronger second-mode response. The results of this work provide a preliminary framework for applying high-fidelity receptivity simulations to the amplitude method for transition prediction in hypersonic flows.
宽频带接受度数据在幅值法过渡预测中的应用
传统的高超音速过渡预测依赖于高度经验的[公式:见正文]方法,该方法基于相对扰动增长的理论近似值。这并没有考虑到接受机制和实验风洞条件中存在的高度可变性,这本身就导致了过渡[公式:见正文]因素的高度可变性。振幅法更接近边界层扰动的宽带性质,以前曾被提出用于考虑接收性的影响。在这项研究中,将马赫数为10的两个钝锥对宽带扰动的高保真度模拟二阶模态接收数据应用于振幅法的迭代近似,该方法针对二阶模态主导流进行了调谐。基于阿诺德工程开发中心9号风洞的实验案例,所研究的几何形状由9.525和5.080-mm直径的7度半角直锥组成。振幅法预测显示,使用标准阈值[公式:见正文]因子的[公式:参见正文]估计的准确性有所提高。特别地,不那么钝的5.080毫米锥体由于其更强的二阶模态响应而表现出最佳一致性。这项工作的结果为将高保真度接收性模拟应用于高超音速流动中跃迁预测的振幅方法提供了初步框架。
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来源期刊
Journal of Spacecraft and Rockets
Journal of Spacecraft and Rockets 工程技术-工程:宇航
CiteScore
3.60
自引率
18.80%
发文量
185
审稿时长
4.5 months
期刊介绍: This Journal, that started it all back in 1963, is devoted to the advancement of the science and technology of astronautics and aeronautics through the dissemination of original archival research papers disclosing new theoretical developments and/or experimental result. The topics include aeroacoustics, aerodynamics, combustion, fundamentals of propulsion, fluid mechanics and reacting flows, fundamental aspects of the aerospace environment, hydrodynamics, lasers and associated phenomena, plasmas, research instrumentation and facilities, structural mechanics and materials, optimization, and thermomechanics and thermochemistry. Papers also are sought which review in an intensive manner the results of recent research developments on any of the topics listed above.
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