DEVELOPMENT OF A COMPUTER BASED LEARNING TOOL FOR UNDERSTANDING AIRCRAFT STRUCTURES
Mazhar, F., Khan, A., Aziz, I. (2007). DEVELOPMENT OF A COMPUTER BASED LEARNING TOOL FOR UNDERSTANDING AIRCRAFT STRUCTURES. EKB Journal Management System, 12(ASAT Conference, 29-31 May 2007), 1-11. doi: 10.21608/asat.2007.24384
Farrukh Mazhar; Abdul Munem Khan; Irfan Aziz. "DEVELOPMENT OF A COMPUTER BASED LEARNING TOOL FOR UNDERSTANDING AIRCRAFT STRUCTURES". EKB Journal Management System, 12, ASAT Conference, 29-31 May 2007, 2007, 1-11. doi: 10.21608/asat.2007.24384
Mazhar, F., Khan, A., Aziz, I. (2007). 'DEVELOPMENT OF A COMPUTER BASED LEARNING TOOL FOR UNDERSTANDING AIRCRAFT STRUCTURES', EKB Journal Management System, 12(ASAT Conference, 29-31 May 2007), pp. 1-11. doi: 10.21608/asat.2007.24384
Mazhar, F., Khan, A., Aziz, I. DEVELOPMENT OF A COMPUTER BASED LEARNING TOOL FOR UNDERSTANDING AIRCRAFT STRUCTURES. EKB Journal Management System, 2007; 12(ASAT Conference, 29-31 May 2007): 1-11. doi: 10.21608/asat.2007.24384

DEVELOPMENT OF A COMPUTER BASED LEARNING TOOL FOR UNDERSTANDING AIRCRAFT STRUCTURES

International Conference on Aerospace Sciences and Aviation Technology
Article 125, Volume 12, ASAT Conference, 29-31 May 2007, May 2007, Page 1-11  XML PDF (583.67 K)
Document Type: Original Article
DOI: 10.21608/asat.2007.24384
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Authors
Farrukh Mazhar1; Abdul Munem Khan2; Irfan Aziz3
1Dept of Industrial Engg, College of Aeronautical Engg, National University of Science and Technology, Rawalpindi, Pakistan.
2Dept of Aerospace Engg, College of Aeronautical Engineering, National University of Science and Technology, Rawalpindi, Pakistan.
3Dept of Mech Engg, University of Engineering and Technology, Peshawar, Pakistan.
Abstract
In today’s engineering design, extensive mathematical calculations / computational analysis are done, which requires powerful engineering software to facilitate and reduce the mathematical workload. This paper pertains to the development of a computer based learning software, named “STATOL®”, for understanding aircraft structures. The software is developed to analyse complex structures used in aircraft constructions, with an aim to facilitate understanding of such problems in a class and enable the user to perform parametric study to appreciate the effect of varying different input on the resultants. The computer code is written in Microsoft Visual Basic 6®.
Keywords
Structures; Aircraft Structures; Shear Flow distribution; software; Computer-based Learning Tool; Theory of Beams
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