Reducing the Sonic Boom Level by Heating the Oncoming Airflow
- 作者: Potapkin A.1, Moskvichev D.1
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隶属关系:
- Khristianovich Institute of Theoretical and Applied Mechanics, Siberian Branch, Russian Academy of Sciences
- 期: 卷 45, 编号 5 (2019)
- 页面: 515-518
- 栏目: Article
- URL: https://journals.rcsi.science/1063-7850/article/view/208319
- DOI: https://doi.org/10.1134/S1063785019050286
- ID: 208319
如何引用文章
详细
We present the results of calculations of the level of sonic boom in the presence of local heating of the airflow in front of a slender body during its supersonic flight in thermal wake behind the heated regions. The Mach number of a cold oncoming airflow was M = 2. Calculations were performed using a combined method of “phantom bodies.” It is established that sequential local heating of the oncoming airflow in two regions in front of the flying body can reduce the sonic boom level by more than 30% as compared to that in the cold airflow.
作者简介
A. Potapkin
Khristianovich Institute of Theoretical and Applied Mechanics, Siberian Branch,Russian Academy of Sciences
编辑信件的主要联系方式.
Email: potapkin@itam.nsc.ru
俄罗斯联邦, Novosibirsk
D. Moskvichev
Khristianovich Institute of Theoretical and Applied Mechanics, Siberian Branch,Russian Academy of Sciences
Email: potapkin@itam.nsc.ru
俄罗斯联邦, Novosibirsk