At the end of this course, the students; 1) Learns flight mechanics, coordinate systems, state variables and equations of motion. 2) Learns external forces and moments, analysis tools, basic design problem and test/prediction tools.
MODE OF DELIVERY
Face to face
PRE-REQUISITES OF THE COURSE
No
RECOMMENDED OPTIONAL PROGRAMME COMPONENT
None
COURSE DEFINITION
Flight Mechanics, Coordinate Systems, State Variables, Equations of Motion, External Forces and Moments: Aerodynamics (Example Aerodynamic Model), Thrust (Example Thrust Model), Gravity, Analysis Tools: Ampiric Tools (Range, Control Effectiveness, Stability), Different Degrees of Freedom Flight Simulations (2dof, 3dof, 6dof), Basic Design Problem: Stability, Control, Range, Dispersion, Test/Prediction Tools: Wind Tunnel Testing, Flight Testing, Computational Methods
Dynamics of Atmospheric Flight, Etkin B., John Wiley&Sons Tactical Missile Design, Fleeman E., AIAA Educational Series Modern Exterior Ballistics, McCoy R.L., Schiffer Military History Tactical and Strategic Missile Guidance, Zarchan Paul, AIAA Tactical Missile Series
PLANNED LEARNING ACTIVITIES AND TEACHING METHODS
Lecture,Questions/Answers,Problem Solving
ASSESSMENT METHODS AND CRITERIA
Quantity
Percentage(%)
Mid-term
1
40
Total(%)
40
Contribution of In-term Studies to Overall Grade(%)
40
Contribution of Final Examination to Overall Grade(%)
60
Total(%)
100
ECTS WORKLOAD
Activities
Number
Hours
Workload
Midterm exam
1
2
2
Preparation for Quiz
Individual or group work
14
4
56
Preparation for Final exam
1
110
110
Course hours
14
3
42
Preparation for Midterm exam
1
90
90
Laboratory (including preparation)
Final exam
1
2
2
Homework
Total Workload
302
Total Workload / 30
10,06
ECTS Credits of the Course
10
LANGUAGE OF INSTRUCTION
Turkish
WORK PLACEMENT(S)
No
KEY LEARNING OUTCOMES (KLO) / MATRIX OF LEARNING OUTCOMES (LO)