^p) 114
g
$»X
t ->-L
if
$G3
^ - ^
mi
ffl
($85 #4 )
57 23 32 20 30
Bf
3
4
B^
3
3
mi
Hi]
B^
ti|
B^
B^
it
4
4
2
2
2
2
128
-^r^
«^ .^t ^
\k • ^^f?c
12
fS.
J ^ J ^ f ^ f (1)
Workshop \ \ \ ~
Practice(l)
Introduction to
Aerospace
1
1
2
2
2
2
2
2
2
^
Engineering
Introduction to
Energy
% i f i 1^
Engineering
1
1
1
2
1
1
2
t f1 •
Graphics
x ^ t f
(2)
Workshop \
Practice(2)
^
f^ ^
;f B M ^ * 1
1 t* 'TW
3
3
3
3
3
3
Mechanical
Materials
3
3
3
Engineering
Mathematics(I)
J
3
3
Applied
% Mechanics(l):
?1^4^fi
Statics
Thermodynamics( I )
Engineering
Mathematics(2)
Applied
Mechanics(2):
11 ^ ^ ' ^ ) "
5.iS.i<fim
•X
3
3
3
3
3
3
3
3
J
Dynamics
Mechanics o f
Materials
Fluid Mechanics
•2
J
Electrical
3
a
J
-1
J
3
3
Engineering
Heat Transfer
Mechatronics
3
3
3
3
3
3
1
3
mtA ' *
(Capstone ^ ; & )
Project on Thermal
Fluid
3
1
3
1
3
i^S*^f^
-
'ft
(Capstone
)
Project on Energy
Engineering
3
1
3
1
3
1
3
3
1
3
1
3
1
3
3
1
3
1
3
1
3
3
1
3
1
3
1
3
3
1
3
1
3
1
3
3
1
3
1
3
1
3
4
6
4
6
4
6
-ft
(Capstone
)
Project on
Mechanical Design
and Manufacturing
(Capstone
)
Project on
Mechatronics and
Aeronautical
Control
-ft
(Capstone Vfi^)
Project on High
sneed G a s
Dynamics
-ft
(Capstone M^^)
Proiect n n Tet
Propulsion
-ft
( Capstone
)
Project on Structure
o f Military Aircraft
1
3 *
43
5
6
14 16 12 12
Computer Aided
Drawing
1
1
2
Experiment o f
Materials
1
1
2
3
3
Mechanical
Dynamics
3
3
3
3
Thermal Fluid
Experiment
1
1
2
Mechanical
Manufacturing
3
3
3
3
3
3
6
6
Mechanical Design
Automatic Control
Thermodynamics
15
5
7
3
3
3
4
5
1
3
3
3
3
3
(2)
Fluid Mechanics
Lab.
1
Aerodynamics
m
3
is.
if Aircraft Structures
z.
2
2
2
2
2
1
1
3
5
7
Principles o f Jet
Propulsion
Flight Mechanics
Aeronautical
Engineering L a b .
\
:
3
3
3
3
3
Unmanned
Aircraft Ground
Systems
x ^ ^ f (4)
3
3
3
Workshop
Practice(4)
1
1
2
15
, 1
x ^ * f
(3)
Workshop
Practice(3)
1
1
2
Introduction to U A S
S w a r m Flight
3
3
3
it
if Introduction to
Unmanned
Aircraft System
7
9
3
3
3
J
a
a
3
3
3
3
3
3
Advanced
Mechanics o f
Materials
3
3
3
Wind Energy
Technology
3
:>
3
Programming
Design
3
3
3
3
3
3
Applied
Mathematics(l)
Vibration
System Dynamics
Advanced
Thermodynamics
i^f
J
# # ; ' 7 ^
$mA^^^
Viscous Fluid
Dynamics
Applications o f
Computer
3
3
3
Applied
Mathematics(2)
3
3
3
Linear Algebra
J
a
Energy Materials
Computational F l u i d
Dynamics
Green Energy
Energy Economics
J
J
a
J
3
3
3
3
3
3
J
-1
3
3
3
3
3
3
Finite Element
Method
3
3
3
The Application o f
Laser Measurement
3
Numerical Analysis
;i^I%tl,x4i
Solar Energy
Engineering
Combustion
3
3
3
3
3
3
3
Refrigeration and
A i r Conditioning
3
3
3
Introduction to
Systems
Engineering
3
3
3
3
3
3"
/•
3
3
3
J
J
3
3
3
3
3
3
3
3
3
3
3
3
Introduction to Fuel
Cell
x t
4.0 4 i W
Industry 4.0
M t x i ^
Micro-ElectroMechanical
Engineering
Introduction to G a s .
Dynamics
Energy Engineering
Renewable Energy
Compressible Fluid
Dynamics
% l x ^
Computer Integrated
Manufacturing and
Smart Factory
Thermal Engines
Heat Treatments
3
3
3
3
3
3
—
Mechanical
Properties o f
Materials
3
3
3
Numerical Control
3
3
3
3
3
3
3
3
3
Computer Aided
Manufacturing
3
3
3
Flexible
3
3
3
Machine
A^mu.
Fluid Machinery
Computer Aided
Design
Manufacture System
3
3
3
3
3
3
tf^m^s/jx-m
3
3
3
3
3
3
3
3
3
3
3
3
3
Performance
Analysis o f Aircraft
and Missile
3
3
3
Introduction to
3
3
3
3
3
3
Introduction to
Bioengineering
Non traditional
Machining
Processes
Computer Aided
Engineering
--
Principles and
Experiments o f
Enhanced Heat
Transfer
3
x7
^ # X ^ ^ ^
Introduction to
Emerging
3
Engineering
fia W/j yj ^ 3
Structural Dynamics
Principles o f
Militaiy Aircraft
Design
A n a l y s i s and Design
o f Military Aircraft
System
special Topics on
it
3
3
3
3
3
3
3
3
3
3
3
3
3
3
3
3
3
Aerodynamics
if Aircraft Propulsion
System
Automatic Control
m
Failure A n a l y s i s o f
Materials
is.
if Theory o f RotatingW i n g Aircraft
^y
Flight Safety
Special Topic on
Aircraft Structures
3
3
3
Satellite Technology
and Application
3
3
3
Flight Control and
Stability
3
3
3
3
3
3
3
3
3
3
Astrodynamics
Composite Materials
Helibome Weapon
Systems
Aircraft
Manufacturing
if
A
^^'^\
i
tf
11
if 128
A'
' A h
-
3
Hypersonic
Aerodynamics
it
3
' -y
i
a«/t#tii-Si*# •
l.*S*aAi7«
SA.S=?-ft
^4r**aB£#
a4tta;feA
X=
ts.«d-(i)(2) • a ^
* - 'f atb^^itia
0 . J€*aAA.
AA*:AA
« f ' a a #
^ tai«)a(i)(2).
»a^aif«t(iu2i
^ ~>
«PfSaftAA
Aa-ifir - B j
*f«?*r.ift'
a a • mrkU
r
if
V.
^
T
if
A -
/XT
S»^A*(1)
(2)
A X
«i4^
> att#
Ara
»A*
ia*.*
m if
X
A =
**ftta:tt
A i
3.*a*yi*iAx
A l * l f e i a • i^ftl
A * * • A-a^
A -
2/^(2)
9&
Jiff A *
X
v^^i^ir^t
A —
1#
/
j!RAa«f?|fc*ti6
jfeAa*tt*ia
ifea&a • « t a «
x a ' Sbifti^ •
*t*(2) ' JRft
Ti^^ife . ;S.,*ti
atai* • *ttf.^f *]•
ltJl^!^t«A* - i
* • i^*ltftA
ft¥*fif4A* >
A * • aAsttt
7.
X^
^
#i^a*<U4t - it
i*5ia* ' 4f^*
tt,*7i • st***#
A -
s*AAW*Ut
AX
* • **;*A
n
ffl • J«M,* •
A X
aan-ra' mm
vi&jR»
^
^
X
^«*&A*
2IL*!(A**J%
AES
J{aai6' Raft
ff't±ft^*f • ftff
^ : ^ a i 6 • ft*M
a * a « - tii^#ifiaaffl • A S A
* '
- ft
ft*if4a^-3fenm^mism •i-ast.*iA* •
fta«La
A*AA'raife
A'
&*^5^i^fe|ia•^^