ABSTRACT

Abstract should state a short introduction of background study, problem statement, purpose of the research, briefing about the used method, principal results and major conclusions. These six items should be included in abstract section (Compulsory). Citation or References and non-standard or uncommon abbreviations should be avoided in the abstract. The number of words should not exceed 350. 

Keywords:

Minimum three keywords; avoid too general and too specific keywords; CDF Letters (Please use semicolon as separator)

1. Introduction ( Capital Letter of Each Word; No indent; Font style: Calibri & Bold; Font Size: 12)

The first sentence should start here [1]. Should have one spacing after section header. The indent of the first line of paragraph should be 0.63cm. Content in body paragraph should be written with the Font style: Calibri; Font size: 12; Paragraph: Justify; Line spacing: 1.0. Important note: Citation cannot stand alone as subject or object. It just as a supportive to a statement. For example, “was also conducted by [4]", should be written as “was also conducted by Uithof et al., [4]” (et al., must be in italic style)

Second paragraph starts here (no spacing between paragraphs).

Generally, in manuscript, should have: 1. Introduction (research background and Literature Review); 2. Methodology; 3. Result; 4. Conclusion; Acknowledgment; References. You may add more if required. The style of the section header as bellow:

1.1 Sub Section Header (Capital Letter of Each Word; No indent; Font style: Calibri & Italic; Font Size: 12)

1.1.1 Sub sub section header (Sentence case; No indent; Font style: Calibri & Italic; Font Size: 12)

Header level three (1.1.1) and above will follow header level three style. No spacing between each header. However, before starting the first paragraph, must have one spacing after the header.

In the last paragraph of the introduction section, Authors should highlight the gap and significant of the research before write the objective of the research. These three items are very important and compulsory.

2. Methodology

2.1 Figure Style and Format

For manuscript publication, all provided Figures must follow the standard of quality for publication. Authors must provide a high quality with high resolution Figure. Content in the Figure should be clear and readable as shown in Figure 1(b) (Especially, the font size of contour legend). For example, as in Figure 1

                                                             (a) (Font style: Calibri; Font size: 10)                             (b)

Fig. 1. Figure quality (a) Unclear and unreadable content (b) Clear and readable content (Font style: calibri; Font size: 11; Paragraph: Align left)

Each Figure must be discussed or mentioned in a body paragraph. The Figure must be placed under the paragraph that discussed about the Figure.

Captions should be below the figure. The caption SHOULD NOT be finished with a full stop (period). The captions should be set to (a) the width of the figure for wider figures (b) centered across the width of the figure, as shown below

                        Note: For long caption

2.2 Table Style and Format

Table should be placed at the center. Each Table must be discussed or mentioned in a body paragraph. The Table must be placed under the paragraph that discussed about the Table. Font style and font size of content in the Table are Calibri and 10, respectively. The content must be align left. The font size of Table caption is 11. The caption SHOULD NOT be finished with a full stop (period). The captions should be set to the width or within of the Table.

Table 1

Place the caption above the table. Here the caption is wider than the table

2.3 Equation Style and Format

All equation that mentioned in body paragraph should be written as Eq. (1). Please use Microsoft Equation in order to present an equation. The font size of equation is 12. Each equation must be numbered as follow

                                                                                                                (1)

3. Results

3.1 XXXX

3.1.1 The effect of XXXX

4. Conclusions

In conclusion part, Author should highlight the finding of their research that respond to the research objective.

Acknowledgement

This research was funded by a grant from Ministry of Higher Education of Malaysia (FRGS Grant R.J130000.7824.4X172).

(Note: This part is compulsory. If this research was not funded by any grant, please write “This research was not funded by any grant”)

References

The list of references should only include works that are cited in the text and that have been published or accepted for publication. Personal communications and unpublished works should only be mentioned in the text. Reference style should be in Chicago style. Please use this link for the DOI number.  Please use reference management software to add references

References (Reference style: Chicago style – must write DOI) Minimum 20 references

[1]        Hummel, D. (2008). Chapter 17 – The International Vortex Flow Experiment 2 (VFE-2): Objectives and Overview. RTO-TR-AVT-113, Page 17-1 – 17-20.

[2]        Luckring, J.M. and Hummel, D. (2008). Chapter 24 – What Was Learned From The New VFE-2 Experiments. RTO-TR-AVT-113. https://doi.org/10.2514/6.2008-383

[3]        Mat, Shabudin Bin, Richard Green, Roderick Galbraith, and Frank Coton. "The effect of edge profile on delta wing flow." Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering 230, no. 7 (2016): 1252-1262. https://doi.org/10.1177/0954410015606939

[4]        Said, Mazuriah, Shabudin Mat, Shuhaimi Mansor, Ainullotfi Abdul-Latif, and Tholudin Mat Lazim. "Reynolds Number Effects on Flow Topology Above Blunt-Edge Delta Wing VFE-2 Configurations." In 53rd AIAA Aerospace Sciences Meeting, p. 1229. 2015. https://doi.org/10.2514/6.2015-1229

[5]        Luckring, James M. "Initial experiments and analysis of blunt-edge vortex flows for VFE-2 configurations at NASA Langley, USA." Aerospace Science and Technology 24, no. 1 (2013): 10-21. https://doi.org/10.1016/j.ast.2012.02.005

[6]                Konrath, Robert, Christian Klein, and Andreas Schröder. "PSP and PIV investigations on the VFE-2 configuration in sub-and transonic flow." Aerospace Science and Technology 24, no. 1 (2013): 22-31. https://doi.org/10.1016/j.ast.2012.09.003

[7]        Fritz, Willy. "Numerical simulation of the peculiar subsonic flow-field about the VFE-2 delta wing with rounded leading edge." Aerospace Science and Technology 24, no. 1 (2013): 45-55. https://doi.org/10.1016/j.ast.2012.02.006

[8]        Chu, J. and Luckring, J.M. (1996). Experimental Surface Pressure Data Obtained on 650 Delta Wing across Reynolds Number and Mach number Ranges. NASA Technical Memorandum 4645. (Sharp-edged report)