Internal Aerodynamic Performance Enhancement for Aircraft with High Maneuver by Designing a Distributed Submerged Inlet

Internal Aerodynamic Performance Enhancement for Aircraft with High Maneuver by Designing a Distributed Submerged Inlet

Submerged inlet has been widely used in UAVs and cruise missiles due to its good stealth characteristics, but it also brings the disadvantage of poor aerodynamic characteristics. Especially in large maneuvering flight, the flow field near the fuselage has a strong unsteady effect, and the total pres...

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Bibliographic Details
Main Authors: Junyao Zhang, Baigang Mi
Format: Article
Language:English
Published: MDPI AG 2023-01-01
Series:Applied Sciences
Subjects:
submerged inlet
large maneuver state
nested mesh
total pressure distortion index
distortion characteristics
hysteresis effect
Online Access:https://www.mdpi.com/2076-3417/13/3/1459

Internet

https://www.mdpi.com/2076-3417/13/3/1459

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