Parametric Design of Aircraft Wing with Curved Leading Edge
Journal Title: Problemy Mechatroniki. Uzbrojenie, lotnictwo, inżynieria bezpieczeństwa - Year 2018, Vol 9, Issue 1
Abstract
In order to ease modelling procedures, eliminate repetitive effort and save time, modern CAD tools offer the ability to automate tasks via a programming language. Moreover, when the design is an iterative process, the automation permits updating the design variables to generate a new model at each iteration. Based on UG/OPEN GRIP functionalities, this paper aims at developing a parametric model of a curved leading edge aircraft wing. The model is built by executing a GRIP program in which wing parameter values can be assigned via a dialog box.<br/><br/>
Authors and Affiliations
Abdelkader BENAOULI, Stanisław KACHEL
Keywords
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- EP ID EP274656
- DOI 10.5604/01.3001.0011.7182
- Views 59
- Downloads 0
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