Abstract
*† ‡ A methodology for improving the quality of high lift system performance prediction within a multidisciplinary preliminary design process is presented. The high lift system geometry is explicitly modeled and a multiple lifting line method is used to compute its aerodynamic characteristics. Computation times are suitable for use in a preliminary design process, and the results for several test cases show good agreement with wind tunnel and/or high fidelity numerical data. In addition, the method allows for further enhancement by using non-linear airfoil polars for interpolation, improving drag prediction and introducing some degree of non-linear aerodynamic behavior.
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.
