Abstract
A high-lift configuration of the civil aircraft including body, wing in high-lift configuration, nacelle and pylon is considered in the present work. Numerical simulations of the flow have been carried out in the framework of Reynolds averaged Navier-Stokes (RANS) equations for Mach number of 0.2. The passive and active flow control methods, which are capable to improve maximal lift of the aircraft, have been considered. The influence of strakes installed on the nacelle and on the body as well as jet blowing on aerodynamic characteristics has been investigated.
Sign-in/Register to access full text options 
Talk to us
Join us for a 30 min session where you can share your feedback and ask us any queries you have
Schedule a callDisclaimer: All third-party content on this website/platform is and will remain the property of their respective owners and is provided on "as is" basis without any warranties, express or implied. Use of third-party content does not indicate any affiliation, sponsorship with or endorsement by them. Any references to third-party content is to identify the corresponding services and shall be considered fair use under The CopyrightLaw.
