Design and development of air intake is one of the most crucial requirements of any air breathing propulsion system. The performance of the intake ultimately decides the performance of the propulsion system and the aircraft as a whole. Intake design affects both internal and external aerodynamic of the aircraft and hence the design problem involves a large number of variables and multiple design requirements. The current study looks into the Aerodynamic design of S-Duct intake for subsonic conditions. The study takes into consideration, two centerline and five Length-to-Offset ratios as parameters for the design. CFD analysis is conducted for all the configurations at multiple angles of attack and the corresponding data is evaluated. Total pressure recovery and Total pressure distortion coefficients are evaluated for all the configurations and the results are discussed.
Aerodynamic Design and Numerical Analysis of S-Duct Intake
Advances in Engineering res
International Conference on Emerging Trends in Engineering ; 2023 ; Hyderabad, India April 28, 2023 - April 30, 2023
Proceedings of the Second International Conference on Emerging Trends in Engineering (ICETE 2023) ; Kapitel : 123 ; 1226-1233
05.11.2023
8 pages
Aufsatz/Kapitel (Buch)
Elektronische Ressource
Englisch
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