id	author	title	date	pages	extension	mime	words	sentence	flesch	summary	cache	txt
american_scientific_journal-4390	Abdul Rahman, Umran; Mustapha, Faizal	Fuselage Surface Pressure Effects due to Wing Interferences	2018	11	.pdf	application/pdf	2443	126	46	Figure 11: Intersection region fuselage surface pressure variation 7. Figure 7: 20, 44, 65, 80, 90 & 95% wing span samplings American Scientific Research Journal for Engineering, Technology, and Sciences (ASRJETS) (2018) Volume 46, No 1, pp 218-228 224 Figure 8: 99% wing span samplings & top wing surface pressure gradients Referring to Figure 7 & 8, although the bottom wing pressure coefficients follow closely with the experimental results, the same couldn’t be said about the top wing.	cache/american_scientific_journal-4390.pdf	txt/american_scientific_journal-4390.txt