PAÜ .:. Eğitim Öğretim Bilgi Sistemi

COURSE INFORMATION

Course Code	Course Title	L+P Hour	Semester	ECTS
SHU 203	MASS AND BALANCE	3 + 0	3rd Semester	4

COURSE DESCRIPTION

Course Level	Associate's Degree
Course Type	Compulsory
Course Objective	The aim of this course is to provide the student with aerodynamic structure, weight calculation and balancing.
Course Content	531/5000 Aircraft and aircraft types, aerodynamic structure and main parts of aircraft, flight control surfaces, forces acting on aircraft, aircraft service equipment, aircraft operation equipment, passenger service equipment, aircraft loading equipment, definition of maximum lift, landing and non-fuel weights of aircraft, calculation of loads, loading types, principles and limitations, center of gravity and equilibrium, methods of calculating load and equilibrium, explanation of terms on loading plan and filling of forms.
Prerequisites	No the prerequisite of lesson.
Corequisite	No the corequisite of lesson.
Mode of Delivery	Face to Face

COURSE LEARNING OUTCOMES

12	Knowledge of numerical analysis methods and aircraft

COURSE'S CONTRIBUTION TO PROGRAM

	PO 01	PO 02	PO 03	PO 04	PO 05	PO 06	PO 07	PO 08	PO 09	PO 10
LO 012	2	1	1	4	1	1	2	2	4	1
Sub Total	2	1	1	4	1	1	2	2	4	1
Contribution	2	1	1	4	1	1	2	2	4	1

ECTS ALLOCATED BASED ON STUDENT WORKLOAD BY THE COURSE DESCRIPTION

Activities	Quantity	Duration (Hour)	Total Work Load (Hour)
Course Duration (14 weeks/theoric+practical)	26	4	104
Total Work Load ECTS Credit of the Course			104 4

COURSE DETAILS

Select Year

	Course Term	No	Instructors
Details	2019-2020 Fall	1	BAHADIR GÖNENÇ

Course Details

Course Code	Course Title	L+P Hour	Course Code	Language Of Instruction	Course Semester
SHU 203	MASS AND BALANCE	3 + 0	1	Turkish	2019-2020 Fall

Course Coordinator	E-Mail	Phone Number	Course Location	Attendance
Lecturer BAHADIR GÖNENÇ	bgonenc@pau.edu.tr		BOMYO A0006	%60

Goals		The aim of this course is to provide the student with aerodynamic structure, weight calculation and balancing.
Content		531/5000 Aircraft and aircraft types, aerodynamic structure and main parts of aircraft, flight control surfaces, forces acting on aircraft, aircraft service equipment, aircraft operation equipment, passenger service equipment, aircraft loading equipment, definition of maximum lift, landing and non-fuel weights of aircraft, calculation of loads, loading types, principles and limitations, center of gravity and equilibrium, methods of calculating load and equilibrium, explanation of terms on loading plan and filling of forms.

Topics

Weeks	Topics
1	Main components of the aircraft, Bernoulli principle, Velocity and Pressure distribution on Wing Profile
2	Composite Aerodynamic Force, Aircraft forces, Moment effect of forces
3	Force balance equations, moment balance equations, roll, pitch and moment for deflection motion
4	Masses that disrupt the moment balance and their distribution in the aircraft, mass acceleration, center of gravity
5	Center of gravity of an object, measuring the center of gravity of an aircraft, moment of force, balance of forces
6	Moment balance, simple moment balance, force and moment balance for aircraft, right hand rule
7	Change of center of gravity in aircraft, Transport coefficient management
8	Midterm exam
9	Simple model for aerodynamic forces in aircraft
10	Aircraft weight definitions
11	Effect of aircraft's center of gravity on aircraft performance
12	Fuel definitions
13	Analysis of mass and balance manual for aircraft
14	Analysis of mass and balance manual for aircraft

Materials

Materials are not specified.

Resources

Course Assessment

Assesment Methods	Percentage (%)	Assesment Methods Title
Final Exam	60	Final Exam
Midterm Exam	40	Midterm Exam

L+P: Lecture and Practice
PQ: Program Learning Outcomes
LO: Course Learning Outcomes

Prospective Student