The Lecture plan of Gas Dynamics and Propulsion,Regulation 2013 is given for the Mechanical Engineering from Anna University,Chennai.
This is the one of the Problematic papers in VIth Semester of BE-Mechanical Engineering. For the syllabus coverage, you can handled more special classes for the even semester because of number of working days are less compared to odd semester
ME 6604 – Gas Dynamics and Jet
Propulsion
Course Plan
Staff Name : ...............................
Class : III Year Mechanical Academic
Year: 2015- 2016 (Even Semester)
S. No
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Topic
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Page No. in the Text Book
|
Teaching Aids
|
No. of Hr
|
Cumulative no. of Hours
|
|
UNIT I BASIC CONCEPTS AND
ISENTROPIC FLOWS
|
||||||
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|
Introduction to the Subject
|
Own notes
|
BB
|
1
|
1
|
|
|
|
Introduction
to compressible flow, Basic definitions in Thermodynamics and fluid Mechanics
|
3-6,16-22
|
BB
|
1
|
2
|
|
|
|
Steady Flow Energy Equation, momentum
equations
|
36-38,62-63,60-61
|
OHP
|
1
|
3
|
|
|
|
stagnation states
|
39-41
|
BB
|
1
|
4
|
|
|
|
Various regions of compressible flow
|
42-43
|
BB
|
1
|
5
|
|
|
|
Reference velocities
|
43-47
|
OHP
|
2
|
7
|
|
|
|
Types of waves, Mach angle and Mach
cone, Effect of Mach number on Compressibility
|
102,106-108,49
|
BB
|
1
|
8
|
|
|
|
Numerical
problems
|
52-56
|
BB
|
3
|
11
|
|
|
|
Class
Test - I
|
-
|
-
|
1
|
12
|
|
|
|
Isentropic
flow through variable ducts- Nozzle and Diffusers
|
69-72, 73-74
|
BB
|
1
|
13
|
|
|
|
Relation
between change in area to Mach number
|
76-78,79-83
|
OHP
|
2
|
15
|
|
|
|
Use
of gas tables with examples
|
89-90
|
BB
|
1
|
16
|
|
|
|
Numerical
problems
|
91-97
|
BB
|
3
|
19
|
|
|
|
Class
Test - II
|
-
|
-
|
1
|
20
|
|
UNIT II FLOW THROUGH DUCTS
|
||||||
|
|
Introduction
to Fanno flow
|
Own
notes
|
BB
|
1
|
21
|
|
|
|
Fanno flow equation and curve
|
211-216
|
OHP, BB
|
1
|
22
|
|
|
|
Variation of properties and mach
number with duct length
|
218-223
|
OHP
|
2
|
24
|
|
|
|
Numerical problems on Fanno flow
|
233-244
|
BB
|
3
|
27
|
|
|
|
Class
Test – III
|
-
|
-
|
1
|
28
|
|
|
|
Introduction to Rayleigh flow
|
Own notes
|
BB
|
1
|
29
|
|
|
|
Rayleigh flow curve and important
remarks
|
247-250
|
BB
|
1
|
30
|
|
|
|
Rayleigh flow relations
|
251-255
|
OHP
|
2
|
32
|
|
|
|
Variation of flow properties and Maximum
heat transfer in Rayleigh flow
|
256-258
|
OHP
|
1
|
33
|
|
|
|
Numerical problems on Rayleigh flow
|
261-264
|
BB
|
3
|
36
|
|
|
|
Class
Test – IV
|
-
|
-
|
1
|
37
|
|
UNIT III NORMAL AND OBLIQUE
SHOCKS
|
||||||
|
|
Introduction
to shock waves
|
Own notes
|
BB
|
1
|
38
|
|
|
|
Types
and conditions for shock
|
Own
notes
|
BB
|
1
|
39
|
|
|
|
Prandtl-Meyer
equation
Impossibility
of rare fraction waves
|
139-141
|
OHP
|
1
|
40
|
|
|
|
Mach
number across the shock
|
141
|
OHP
|
1
|
41
|
|
|
|
Static
properties across the shock
|
142-146
|
OHP
|
2
|
43
|
|
|
|
Stagnation
properties across the shock
|
146-149
|
OHP
|
2
|
45
|
|
|
|
Class Test – V
|
-
|
-
|
1
|
46
|
|
|
|
Supersonic
wind tunnels, Use of gas tables
|
153-157
|
BB
|
1
|
47
|
|
|
|
Numerical
problems
|
161-170
|
BB
|
3
|
50
|
|
|
|
Introduction
to oblique shock waves
|
174-176
|
OHP,BB
|
1
|
51
|
|
|
|
Flow
with oblique shock waves Relations
|
177-179
|
OHP
|
1
|
52
|
|
|
|
Variation
of Flow Parameters
|
183-187
|
OHP
|
2
|
54
|
|
|
|
Numerical
problems
|
204-208
|
BB
|
3
|
57
|
|
|
|
Class Test – VI
|
-
|
-
|
1
|
58
|
|
UNIT IV JET PROPULSION
|
||||||
|
|
Introduction
to Jet propulsion
|
357-359
|
PPT
|
1
|
59
|
|
|
|
Types
of jet propulsive systems
|
359-363
|
BB
|
1
|
60
|
|
|
|
Turbo
jet engine and turbo prop engine
|
363-366
|
PPT
|
1
|
61
|
|
|
|
Ram
jet engine and Pulse jet engine
|
380-385
|
PPT
|
1
|
62
|
|
|
|
Class Test – VII
|
-
|
-
|
1
|
63
|
|
|
|
Energy
relations equations
|
366-368
|
OHP
|
1
|
64
|
|
|
|
Thrust
Power and efficiencies
|
373-379
|
BB
|
1
|
65
|
|
|
|
Numerical Problems
|
386-392
|
BB
|
3
|
68
|
|
|
|
Class Test – VIII
|
-
|
-
|
1
|
69
|
|
UNIT V SPACE PROPULSION
|
||||||
|
|
Introduction
to rocket propulsion
|
396-398
|
PPT
|
1
|
70
|
|
|
|
Types
of Rocket Engine - Propellants
|
398-407
|
PPT
|
2
|
72
|
|
|
|
Feeding
system
|
407-410
|
PPT
|
1
|
73
|
|
|
|
Ignition
and combustion
|
411-413,415-421
|
PPT
|
1
|
74
|
|
|
|
Class Test – IX
|
-
|
-
|
1
|
75
|
|
|
|
Theory
of rocket propulsion- Performance study
|
421-425
|
BB
|
1
|
76
|
|
|
|
Terminal and
characteristic
Velocity,
Power and efficiencies
|
426-431
|
BB
|
1
|
77
|
|
|
|
Rocket
Engine Applications, Space flight
|
431-435
|
PPT
|
1
|
78
|
|
|
|
Numerical Problems
|
448-455
|
BB
|
2
|
80
|
|
|
|
Class Test – X
|
-
|
-
|
1
|
81
|
|
TEXT
BOOK: S.M.
Yahya, fundamentals of Compressible Flow, New Age International (P) Limited,
New Delhi, 1996.
(Approved Gas Tables is Permitted for the Examinations)
(Approved Gas Tables is Permitted for the Examinations)
ME6604 GDJP-Download all 5 units question bank
Unit 1 Question bank-Click the link
http://annaunivstudymaterials.blogspot.com/2015/11/me6604-gas-dynamics-and-jet-propulsion_27.html
Unit 2 Question bank-Click the link
http://annaunivstudymaterials.blogspot.com/2015/11/me6604-gas-dynamics-and-jet-propulsion_91.html
Unit 3 Question bank-Click the link
http://annaunivstudymaterials.blogspot.com/2015/11/me6604-gas-dynamics-and-jet-propulsion_18.html
Unit 4 Question bank-Click the link
http://annaunivstudymaterials.blogspot.com/2015/11/gas-dynamics-and-jet-propulsion.html
Unit 5 Question bank-Click the link
http://annaunivstudymaterials.blogspot.com/2015/11/university-questions-gas-dynamics-and.html
For more Mechanical Engineering subjects Study materials were uploaded in annaunivstudymaterials.blogspot.com
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