Sensitivity of scale resolving aft-body flow simulations to numerical model parameter variations

Author:

Schumann Jan-Erik,Hannemann Volker,Hannemann Klaus

Abstract

AbstractThe sensitivity of hybrid RANS-LES methods like Improved Delayed Detached Eddy Simulation (IDDES) to numerical model parameter variations related to generic space launch vehicle aft-body flows is investigated. In particular, the changes resulting from the choice of the time-step size, the turbulence model, the fluid modelling, the circumferential grid resolution, the filter length definition, and the data collection period is considered. The results are also compared to experimental and numerical data taken from the available literature. The sensitivity to the time-step size and the turbulence model is minuscule with respect to the obtained mean flow field, wall pressure distributions, azimuthal modes, and wall pressure frequency spectra. However, circumferential resolution, fluid model, and filter length definition affect the solution to a higher extent. Buffeting spectra are very sensitive to the data collection period.

Funder

deutsche forschungsgemeinschaft

Deutsches Zentrum für Luft- und Raumfahrt e. V. (DLR)

Publisher

Springer Science and Business Media LLC

Subject

Space and Planetary Science,Aerospace Engineering

Reference25 articles.

1. Capitelli, M., Colonna, G., Marraffa, L.: Tables of internal partition functions and thermodynamic properties of high-temperature Mars-atmosphere species from 50K to 50000K. ESA Scientific Technical Review 246 (2005)

2. Chauvet, N., Deck, S., Jacquin, L.: Zonal detached eddy simulation of a controlled propulsive jet. AIAA J. 45(10), 2458–2473 (2007)

3. Deck, S., Thorigny, P.: Unsteadiness of an axisymmetric separating-reattaching flow: numerical investigation. Phys. Fluids 19(6), 065103 (2007)

4. Deprés, D., Reijasse, P., Dussauge, J.: Analysis of unsteadiness in afterbody transonic flows. AIAA J. 42(12), 2541–2550 (2004)

5. Fertig, M., Schumann, J.E., Hannemann, V., Eggers, T., Hannemann, K.: Steps towards the accurate simulation of launch vehicle base flows with hot plumes. In: Stemmer, C., Adams, N.A., Haidn, O.J., Radespiel, R., Sattelmayer, T., Schröder, W., Weigand, B. (eds.) SFB/TRR 40 annual report 2019. Technische Universität München, Lehrstuhl für Aerodynamik und Strömungstechnik (2019)

Cited by 1 articles. 订阅此论文施引文献 订阅此论文施引文献,注册后可以免费订阅5篇论文的施引文献,订阅后可以查看论文全部施引文献

同舟云学术

1.学者识别学者识别

2.学术分析学术分析

3.人才评估人才评估

"同舟云学术"是以全球学者为主线,采集、加工和组织学术论文而形成的新型学术文献查询和分析系统,可以对全球学者进行文献检索和人才价值评估。用户可以通过关注某些学科领域的顶尖人物而持续追踪该领域的学科进展和研究前沿。经过近期的数据扩容,当前同舟云学术共收录了国内外主流学术期刊6万余种,收集的期刊论文及会议论文总量共计约1.5亿篇,并以每天添加12000余篇中外论文的速度递增。我们也可以为用户提供个性化、定制化的学者数据。欢迎来电咨询!咨询电话:010-8811{复制后删除}0370

www.globalauthorid.com

TOP

Copyright © 2019-2024 北京同舟云网络信息技术有限公司
京公网安备11010802033243号  京ICP备18003416号-3