Identyfikatory
Warianty tytułu
Języki publikacji
Abstrakty
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.
Rocznik
Strony
93--104
Opis fizyczny
Bibliogr. 9 poz., rys., wykr.
Twórcy
autor
- Military University of Technology, Faculty of Mechatronics and Aerospace, 2 Urbanowicza Str., 00-908 Warsaw, Poland
autor
- Military University of Technology, Faculty of Mechatronics and Aerospace, 2 Urbanowicza Str., 00-908 Warsaw, Poland
Bibliografia
- [1] Asiedu Y., P. Gu. 1998. "Product life cycle cost analysis: state of the art review". International Journal of Production Research 36 (4) : 883-908.
- [2] McMasters J.H., R. M. Cummings. 2004. Rethinking the Airplane Design Process – An Early 21st Century Perspective. AIAA 2004-693, 42nd AIAA Aerospace Sciences Meeting and Exhibit, Reno, NV, USA.
- [3] Amadori Kristian. 2012. Geometry based design automation: applied to aircraft modelling and optimization. PhD diss., Linköping University Electronic Press.
- [4] Zaware B. Atul, M. M. Mirza. 2015. Customization of UG NX software for 3D modelling of Fins. Presented at National Conference for Engineering Post Graduates RIT NConPG – 15, June 2015.
- [5] Palekar Jayesh, H. P. Khairnar, M. Tech Cad Cam. 2014 "Master Model Automation Using NX Unigraphics Customization". International Journal of Engineering Development and Research 2 (2) : 2184-2189.
- [6] Azamatov Abdulaziz, Jae-Woo Lee, Yung-Hwan Byun. 2011. "Comprehensive aircraft configuration design tool for integrated product and process development." Advances in engineering software 42 : 35-49.
- [7] Kachel Stanisław. 2013. “Optimization of wing parameters to achieve minimum weight at defined aerodynamic loads”. Journal of Theoretical and Applied Mechanics 51 (1) : 159-170.
- [8] Kachel Stanisław, Adam Kozakiewicz, Stanisław Wrzesień. 2015. The process control of design for integration CAD/CAE system for static and dynamic analysis of the fanner. Presented at The 2nd International SPDM Conference, San Diego.
- [9] Unigraphics Solutions Inc. GRIP Fundamentals - Student Guide, November 2003.
Uwagi
Opracowanie rekordu w ramach umowy 509/P-DUN/2018 ze środków MNiSW przeznaczonych na działalność upowszechniającą naukę (2018).
Typ dokumentu
Bibliografia
Identyfikator YADDA
bwmeta1.element.baztech-cbda83ba-b719-4855-b6d7-02ff439f6712