“Computational Fluid Dynamics Analysis of the Infrared Emission from a Generic Hypersonic Glide Vehicle”—A Response

IF 0.7 Q3 INTERNATIONAL RELATIONS
C. Tracy, David Wright
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引用次数: 0

Abstract

Abstract A recent paper by Candler and Leyva in Science & Global Security comments on our 2020 paper “Modelling the Performance of Hypersonic Boost-Glide Missiles” analyzing the capabilities of hypersonic boost-glide weapons. They provide useful new data on several previously uncertain aspects of glide vehicle aerodynamics and report results from computational fluid dynamics calculations of heating and infrared light emission from hypersonic vehicles during the glide phase. They report infrared emissions lower than those we reported but still above the minimum detection threshold of modern U.S. space sensors. We discuss how Candler and Leyva’s new data can be incorporated into our analytical model and identify significant, unresolved discrepancies between their results and those of a previously published computational fluid dynamics analysis of the same glide vehicle. Finally, we comment on the role of social processes in the construction of knowledge about hypersonic weapon performance.
“通用高超声速滑翔飞行器红外发射的计算流体动力学分析”-响应
Candler和Leyva最近在《科学与全球安全》上发表的一篇论文对我们2020年的论文《高超声速助推滑翔导弹的性能建模》进行了评论,该论文分析了高超声速助推滑翔武器的能力。他们为滑翔飞行器空气动力学的几个先前不确定的方面提供了有用的新数据,并报告了高超声速飞行器在滑翔阶段加热和红外光发射的计算流体动力学计算结果。他们报告的红外辐射比我们报告的要低,但仍高于现代美国空间传感器的最低探测阈值。我们讨论了如何将Candler和Leyva的新数据纳入我们的分析模型,并确定他们的结果与先前发表的相同滑翔飞行器的计算流体动力学分析之间的重大未解决的差异。最后,我们评论了社会过程在构建高超声速武器性能知识中的作用。
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
Science & Global Security
Science & Global Security INTERNATIONAL RELATIONS-
CiteScore
1.00
自引率
14.30%
发文量
8
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