Akademik Dersler - İçerik

0 : Does not support 1 : Low-level support 2 : Mid-level support 3 : Top level support

Learning Outcomes	1	2	3	4	5	6	7	8	9	10	11	12	13	14
Determine the pressure, the temperature and the density of the air at the specified altitude	-	-	-	-	-	-	-	-	-	-	-	-	-	-
Understand how the head wind and the tail wind change the ground velocity of the aircraft	-	-	-	-	-	-	-	-	-	-	-	-	-	-
Explain characteristics of boundary layer composition caused by changes in friction and wing airfoil shape.	-	-	-	-	-	-	-	-	-	-	-	-	-	-
Compute stall speed and changes to stall speed due to variables such as weight load factor, altitude and lift coefficient.	-	-	-	-	-	-	-	-	-	-	-	-	-	-
Examine the differences between the wing and the airfoil.	-	-	-	-	-	-	-	-	-	-	-	-	-	-
Understand how the altitude change effects the drag and the thrust of the aircraft	-	-	-	-	-	-	-	-	-	-	-	-	-	-
Examines how the wing tip vorticies occurs and what it effects	-	-	-	-	-	-	-	-	-	-	-	-	-	-
Learn the types of Shock Waves and the ways to minimize its effects on the aircraft	-	-	-	-	-	-	-	-	-	-	-	-	-	-
Understand how the center of gravity of the aircraft has an important role on the aircraft\'s stability	-	-	-	-	-	-	-	-	-	-	-	-	-	-