Study on Aerodynamic Design of the Front Auxiliary Inlet
Submerged inlets have been widely used in advanced aircraft due to their excellent stealth characteristics, but they also suffer from poor aerodynamic performance. To improve the aerodynamic efficiency while maintaining stealth capabilities, this paper proposes a design scheme for a front auxiliary...
Main Authors: | Junyao Zhang, Hao Zhan, Baigang Mi |
---|---|
Format: | Article |
Language: | English |
Published: |
MDPI AG
2023-08-01
|
Series: | Aerospace |
Subjects: | |
Online Access: | https://www.mdpi.com/2226-4310/10/8/700 |
Similar Items
-
Numerical Investigation of a Vortex Diverter Designed for Improving the Performance of the Submerged Inlet
by: Junyao Zhang, et al.
Published: (2023-12-01) -
Internal Aerodynamic Performance Enhancement for Aircraft with High Maneuver by Designing a Distributed Submerged Inlet
by: Junyao Zhang, et al.
Published: (2023-01-01) -
Prepositive Synergistic Bulge Design for Improving Aerodynamic Performance of Submerged Inlet
by: Xuan Bai, et al.
Published: (2023-07-01) -
Numerical Simulations Study on the Effect of Propeller Slipstream on Inlet Flow Field for a Turboprop Aircraft
by: WANG Limin, et al.
Published: (2020-06-01) -
Improving the efficiency of a serpentine inlet duct by using of Blowing Jet Vortex Generators flow control technique
by: iman Maghsoudi, et al.
Published: (2018-06-01)