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.
Mathematical Modeling of Interferential Flow around the Finned Body in the Transport Compartment and When Exiting Thereof at Subsonic Aircraft Movement
Russ. Aeronaut.
Russian Aeronautics ; 64 , 4 ; 678-687
2021-10-01
10 pages
Aufsatz (Zeitschrift)
Elektronische Ressource
Englisch
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