Parametryczne projektowanie skrzydła samolotu z krzywoliniową krawędzią natarcia ; Parametryczne projektowanie skrzydła samolotu z krzywoliniową krawędzią natarcia
Stanisław KACHEL ; Stanisław KACHEL
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.
;
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.
Warszawa
;
Warszawa
Wojskowa Akademia Techniczna ; Wojskowa Akademia Techniczna
oai:ribes-88.man.poznan.pl:2495
DOI 10.5604/01.3001.0011.7182 ; DOI 10.5604/01.3001.0011.7182
Wojskowa Akademia Techniczna ; Wojskowa Akademia Techniczna
mechanics, modelling of air-structures, Siemens NX systems, GRIPl anguage for Siemens NX system ; mechanics, modelling of air-structures, Siemens NX systems, GRIPl anguage for Siemens NX system
16 wrz 2025
16 wrz 2025
0
https://ribes-88.man.poznan.pl/publication/2803
| Nazwa wydania | Data |
|---|---|
| Parametric Design of Aircraft Wing with Curved Leading Edge | 16 wrz 2025 |