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Application of Mathematical Modeling to Study Near-Field Pressure Pulsations of a Near-Future Prototype Supersonic Business Aircraft
Journal of Aerospace Engineering ( IF 2.4 ) Pub Date : 2021-10-18 , DOI: 10.1061/(asce)as.1943-5525.0001373 A. S. Kozelkov 1 , D. Yu. Strelets 2 , M. S. Sokuler 3 , R. H. Arifullin 3
Journal of Aerospace Engineering ( IF 2.4 ) Pub Date : 2021-10-18 , DOI: 10.1061/(asce)as.1943-5525.0001373 A. S. Kozelkov 1 , D. Yu. Strelets 2 , M. S. Sokuler 3 , R. H. Arifullin 3
Affiliation
The paper considers practical aspects of mathematical modeling in predictions of the
level of near-field pressure pulsations of a near-future prototype supersonic business
aircraft. A numerical modeling technique based on the numerical solution of ...
中文翻译：
应用数学建模研究未来原型超音速公务机近场压力脉动
本文考虑了数学建模在预测近期超音速商务飞机原型机的近场压力脉动水平方面的实际应用。一种基于...数值解的数值建模技术
更新日期：2021-10-19
中文翻译：
应用数学建模研究未来原型超音速公务机近场压力脉动
本文考虑了数学建模在预测近期超音速商务飞机原型机的近场压力脉动水平方面的实际应用。一种基于...数值解的数值建模技术
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