俄罗斯空气动力研究所中心学报
每年出版 6 期
ISSN 打印: 1948-2590
ISSN 在线: 1948-2604
DEVELOPMENT OF THE CONCEPT OF CURVILINEAR CHANNELS FOR PROPULSION SYSTEM INLETS AND NOZZLES EMBEDDED IN THE AIRFRAME
卷 47,
册 7, 2016,
pp. 747-758
DOI: 10.1615/TsAGISciJ.2017019841
摘要
The propulsion airframe integrated configuration of a tailless aircraft is considered in this study. Several concepts of embedded inlets and nozzles are presented. The results of the numerical flow simulation in the presented inlets and nozzles are obtained.
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