Research on Unsteady Flow Field Characteristics of Submerged Inlet under Large Maneuver Condition

Research on Unsteady Flow Field Characteristics of Submerged Inlet under Large Maneuver Condition

In order to explore the differences in steady-state and transient aerodynamic characteristics of submerged inlets during high maneuvering flight, this study focuses on cruise missile and adopts CFD numerical methods to conduct steady-state and transient analysis of the submerged inlets. The research...

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Podrobná bibliografie
Hlavní autor: Feng Yuhua, Zhang Junyao, Wang Limin, Mi Baigang
Médium: Článek
Jazyk:zho
Vydáno: Editorial Office of Aero Weaponry 2024-06-01
Edice:Hangkong bingqi
Témata:
|submerged inlet|large maneuvering state|nested grid|total pressure distortion index|distortion characteristics|hysteresis effect
On-line přístup:https://www.aeroweaponry.avic.com/fileup/1673-5048/PDF/2023-00128.pdf

Internet

https://www.aeroweaponry.avic.com/fileup/1673-5048/PDF/2023-00128.pdf

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