Parametric Design of Aircraft Wing with Curved Leading Edge

• Autorzy: Benaouali A. , Kachel S.

Identyfikatory

DOI

10.5604/01.3001.0011.7182

• Języki publikacji: EN

Abstrakty

EN

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.

Słowa kluczowe

EN

mechanics; modelling of air-structures; Siemens NX systems; GRIP language for Siemens NX system

• Wydawca: Wojskowa Akademia Techniczna im. Jarosława Dąbrowskiego
• Czasopismo: Problemy Mechatroniki : uzbrojenie, lotnictwo, inżynieria bezpieczeństwa
• Rocznik: 2018
• Tom: Vol. 9, Nr 1 (31)
• Strony: 93--104
• Opis fizyczny: Bibliogr. 9 poz., rys., wykr.

Twórcy

autor

Benaouali A.

• Military University of Technology, Faculty of Mechatronics and Aerospace, 2 Urbanowicza Str., 00-908 Warsaw, Poland

autor

Kachel S.

• 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).