id	author	title	date	pages	extension	mime	words	sentence	flesch	summary	cache	txt
alkej-542	Ismail, Laith W.	بحث توزيع الحمل والضغط على الجناح مع التفاف دوامات الأثر لطائرة ذات سرعة واطئة	2018	10	.pdf	application/pdf	3374	155	68	The capability of the present method is investigated through a number of test cases with different types of wing sections (NACA 0012 and GA(W)-1) for different aspect ratios and angles of attack, the results include the lift and drag curves, lift and pressure distributions along the wing span taking into the consideration the effect of the angles of attack and the aspect ratios on the wake rollup. Pressure Distribution on the Upper Surface of Wing with NACA 0012 (a) AR=3 (b) AR=4.	cache/alkej-542.pdf	txt/alkej-542.txt