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Title: Parametric Design of Aircraft Wing with Curved Leading Edge
Alternative title:
Parametryczne projektowanie skrzydła samolotu z krzywoliniową krawędzią natarcia
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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.
Place of publishing:
Warszawa
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Identifier:
oai:ribes-88.man.poznan.pl:2495
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Keywords:
mechanics, modelling of air-structures, Siemens NX systems, GRIPl anguage for Siemens NX system
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Last modified:
Sep 16, 2025
In our library since:
Sep 16, 2025
Number of object content hits:
0
All available object's versions:
https://ribes-88.man.poznan.pl/publication/2803
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| Edition name | Date |
|---|---|
| Parametric Design of Aircraft Wing with Curved Leading Edge | Sep 16, 2025 |
