@misc{Abdelkader_BENAOUALI_Parametric_2018-03-31,
 author={Abdelkader BENAOUALI and Abdelkader BENAOUALI},
 copyright={Wojskowa Akademia Techniczna},
 copyright={Wojskowa Akademia Techniczna},
 address={Warszawa},
 address={Warszawa},
 howpublished={online},
 year={2018-03-31},
 year={2018-03-31},
 publisher={Wojskowa Akademia Techniczna},
 publisher={Wojskowa Akademia Techniczna},
 language={angielski},
 language={angielski},
 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.},
 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.},
 type={artykuł},
 type={artykuł},
 title={Parametric Design of Aircraft Wing with Curved Leading Edge},
 title={Parametric Design of Aircraft Wing with Curved Leading Edge},
 keywords={Projektowanie skrzydłą samolotu, Projektowanie skrzydłą samolotu},
}