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Mathematical Modeling of Interferential Flow around the Finned Body in the Transport Compartment and When Exiting Thereof at Subsonic Aircraft Movement
     
  
  
刊名:
Russian Aeronautics
作者:
Tokareva P. V.
(AO GNPP “Region”)
Grumondz V. T.
(Moscow Aviation Institute (National Research University))
Kalugin V. T.
(Bauman Moscow State Technical University)
刊号:
877B0298
ISSN:
1068-7998
出版年:
2021
年卷期:
2021, vol.64, no.4
页码:
678-687
总页数:
10
分类号:
V2
关键词:
mathematical modeling
;
interference flow
;
finned body of revolution
;
exit from the transport compartment
参考中译:
语种:
eng
文摘:
The paper considers the mathematical modeling of the air flow in an empty transport compartment at a subsonic speed of the aircraft at various angles of flaps opening, as well as the flow in a cluttered compartment in the presence of a finned body of revolution placed in it. The modeling of interference flow processes around a finned body of revolution at the exit from the transport compartment was carried out.
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