Effects of mesh resolution on hypersonic heating prediction

التفاصيل البيبلوغرافية
العنوان: Effects of mesh resolution on hypersonic heating prediction
المؤلفون: 孙泉华, 朱辉玉, 王刚, 樊菁
سنة النشر: 2011
المجموعة: IMECH-IR (Institute of Mechanics, Chinese Academy of Sciences) / 中国科学院力学研究所机构知识库
مصطلحات موضوعية: Hypersonic Flow, Aeroheating, Cfd, Mesh Resolution, 流体力学::空气动力学, 流体力学::稀薄气体力学, 流体力学::计算流体力学, computational fluid dynamics, 超声速流[动], 超音速流动, 超声速流动, 高速流, 高超声速流动, supersonic flow, supersonics, 超音速流[动], 高超音速流[动], 高超声速流[动], ecoulement hypersonique, fliessen bei ueberschallgeschwindigkeit, hypersonics, 计算流体力学, computational fluid mechanics, materials science computing, mechanical engineering computing, physics computing, charge flow devices, computational aerodynamics
الوصف: Aeroheating prediction is a challenging and critical problem for the design and optimization of hypersonic vehicles. One challenge is that the solution of the Navier-Stokes equations strongly depends on the computational mesh. In this letter, the effect of mesh resolution on heat flux prediction is studied. It is found that mesh-independent solutions can be obtained using fine mesh, whose accuracy is confirmed by results from kinetic particle simulation. It is analyzed that mesh-induced numerical error comes mainly from the flux calculation in the boundary layer whereas the temperature gradient on the surface can be evaluated using a wall function. Numerical schemes having strong capability of boundary layer capture are therefore recommended for hypersonic heating prediction
نوع الوثيقة: report
اللغة: English
Relation: Theoretical & Applied Mechanics letters; Sun QH,Zhu HY,Wang G,et al. Effects of mesh resolution on hypersonic heating prediction[J]. Theoretical & Applied Mechanics letters,2011,1:022001.; http://dspace.imech.ac.cn/handle/311007/46974; http://taml.cstam.org.cn/EN/Y2011/V1/I2/9
الاتاحة: http://dspace.imech.ac.cn/handle/311007/46974
http://taml.cstam.org.cn/EN/Y2011/V1/I2/9
رقم الانضمام: edsbas.65473CDC
قاعدة البيانات: BASE