Possibilities of Simplified Numerical Modeling of the Stardust Sample Descent Capsule Flight

IF 0.7 4区工程技术 Q4 MECHANICS

Fluid Dynamics Pub Date : 2026-09-04 DOI:10.1134/S0015462826605425

V. Batygina

引用次数: 0

Abstract

The flight of the Stardust descent capsule is examined. The possibility of simplified calculation of the capsule flow is studied using the perfect gas model when varying the specific heat ratio in the NERAT-2D software. This assumption makes it possible to quickly obtain the accurate flow pattern over a certain altitude range, but often it underestimates the heat flux to the capsule surface.

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星尘号样品降落舱飞行简化数值模拟的可能性

对星尘号下降舱的飞行进行了检查。研究了在NERAT-2D软件中采用理想气体模型改变比热比时简化胶囊流动计算的可能性。这种假设可以快速获得一定高度范围内的精确流型，但往往低估了到达太空舱表面的热通量。

本文章由计算机程序翻译，如有差异，请以英文原文为准。

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来源期刊

Fluid Dynamics MECHANICS-PHYSICS, FLUIDS & PLASMAS

CiteScore

1.30

自引率

22.20%

发文量

审稿时长

6-12 weeks

期刊介绍： Fluid Dynamics is an international peer reviewed journal that publishes theoretical, computational, and experimental research on aeromechanics, hydrodynamics, plasma dynamics, underground hydrodynamics, and biomechanics of continuous media. Special attention is given to new trends developing at the leading edge of science, such as theory and application of multi-phase flows, chemically reactive flows, liquid and gas flows in electromagnetic fields, new hydrodynamical methods of increasing oil output, new approaches to the description of turbulent flows, etc.