EG-M69, Advanced Airframe Structure, Assignment 1 Report Preparation Instructions 25-26

Q1

1.1  Results and discussion

Please include the results of Q1 and discussion of these results in this section. Make sure you use table/figure to show the results. It is very important to use caption, table/figure number that you can refer to them in the following subsection.

Figures and tables must be numbered consecutively. Each figure and table (e.g. table 1) should have a caption. Place captions on or near the illustrations, at the bottom. Use small captions. The most convenient place for figures is at the top of a page. The styles Figure and Captions, provided in this template, will assure the correct spacing between tables, figures and the text. Otherwise, insert a vertical space of 34pt between the actual text and figure (or table) including the caption.

Q2

2.1 Results and discussion

Please include the results of Q2 and discussion of these results in this section. Make sure you use table/figure to show the results. It is very important to use caption, table/figure number that you can refer to them in the following subsection. 

Q3

3.1 Results and discussion

Please include the results of Q3 and discussion of these results in this section. Make sure you use table/figure to show the results. It is very important to use caption, table/figure number that you can refer to them in the following subsection.

Q4

Results and discussion

Please include the results of Q4 and discussion of these results in this section. Make sure you use table/figure to show the results. It is very important to use caption, table/figure number that you can refer to them in the following subsection. 

References

References should be quoted in the text between square brackets (e.g. [1]). The formats for the references to books [1], journal papers [2] and publications in proceedings [3] and lecture notes [4] are shown at the end of these instructions.
References

[1]T.H.G. Megson, Aircraft Structures for Engineering Students, Elsevier Ltd, (2012).

[2]H. Haddad Khodaparast, J.E. Cooper, Rapid Prediction of Worst-Case Gust Loads Following Structural Modification, AIAA Journal, Vol. 52, No. 2, (2014), pp. 242-254.

[3]K.J. Badcock, H. Haddad Khodaparast, S. Timme, J.E. Mottershead, Calculating the Influence of Structural Uncertainty on Aeroelastic Limit Cycle Response, Proceedings of 52ND AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics and Material Conference, Denver, Orlando,2011 April 4-7, pp. 1-16.

[4]H. Haddad Khodaparast, Buckling in Aircraft Structures, EGM69-Advanced Airframe Structures Lecture notes, Faculty of Science and Engineering, Swansea University, Fall 2020.