SEMESTER VII SEVENTH SEMESTER AERONAUTICAL ENGINEERING ANNA UNIVERSITY CHENNAI SYLLABUS
SEMESTER VII SEVENTH SEMESTER AERONAUTICAL ENGINEERING ANNA UNIVERSITY CHENNAI SYLLABUS
SEMESTER VII
THEORY
GE2022 Total Quality Management
AE2401 Avionics
AE2402 Computational Fluid Dynamics
AE2403 Vibrations And Elements of Aero elasticity
Elective – II
Elective – III
PRACTICAL
AE2404 Aircraft Design Project - II 0 0 3 2
AE2405 Aircraft Systems Laboratory 0 0 3 2
AE2406 Avionics Laboratory 0 0 3 2
AE2407 Identification of Project Work 0 0 2 1
TOTAL 18 0 11 25
2
GE2022 TOTAL QUALITY MANAGEMENT L T P C
(Common to all branches)
OBJECTIVE
• To understand the Total Quality Management concept and principles and the various
tools available to achieve Total Quality Management.
• To understand the statistical approach for quality control.
• To create an awareness about the ISO and QS certification process and its need for
the industries.
UNIT I INTRODUCTION 9
Definition of Quality, Dimensions of Quality, Quality Planning, Quality costs - Analysis
Techniques for Quality Costs, Basic concepts of Total Quality Management, Historical
Review, Principles of TQM, Leadership – Concepts, Role of Senior Management,
Quality Council, Quality Statements, Strategic Planning, Deming Philosophy, Barriers to
TQM Implementation.
UNIT II TQM PRINCIPLES 9
Customer satisfaction – Customer Perception of Quality, Customer Complaints, Service
Quality, Customer Retention, Employee Involvement – Motivation, Empowerment,
Teams, Recognition and Reward, Performance Appraisal, Benefits, Continuous Process
Improvement – Juran Trilogy, PDSA Cycle, 5S, Kaizen, Supplier Partnership –
Partnering, sourcing, Supplier Selection, Supplier Rating, Relationship Development,
Performance Measures – Basic Concepts, Strategy, Performance Measure.
UNIT III STATISTICAL PROCESS CONTROL (SPC) 9
The seven tools of quality, Statistical Fundamentals – Measures of central Tendency
and Dispersion, Population and Sample, Normal Curve, Control Charts for variables and
attributes, Process capability, Concept of six sigma, New seven Management tools.
UNIT IV TQM TOOLS 9
Benchmarking – Reasons to Benchmark, Benchmarking Process, Quality Function
Deployment (QFD) – House of Quality, QFD Process, Benefits, Taguchi Quality Loss
Function, Total Productive Maintenance (TPM) – Concept, Improvement Needs, FMEA –
Stages of FMEA.
10
UNIT V QUALITY SYSTEMS 9
Need for ISO 9000 and Other Quality Systems, ISO 9000:2000 Quality System –
Elements, Implementation of Quality System, Documentation, Quality Auditing, TS
16949, ISO 14000 – Concept, Requirements and Benefits.
TOTAL: 45 PERIODS
TEXT BOOK
1. Dale H.Besterfiled, et al., “Total Quality Management”, Pearson Education, Inc.
2003. (Indian reprint 2004). ISBN 81-297-0260-6.
REFERENCES
1. Evans. J. R. & Lindsay. W,M “The Management and Control of Quality”, (5th Edition),
South-Western (Thomson Learning), 2002 (ISBN 0-324-06680-5).
2. Feigenbaum.A.V. “Total Quality Management”, McGraw-Hill, 1991.
3. Oakland.J.S. “Total Quality Management”, Butterworth Hcinemann Ltd., Oxford,
1989.
4. Narayana V. and Sreenivasan, N.S. “Quality Management – Concepts and Tasks”,
New Age International 1996.
5. Zeiri. “Total Quality Management for Engineers”, Wood Head Publishers, 1991.
AE2401 AVIONICS L T P C
OBJECTIVE
To introduce the basic concepts of navigation & communication systems of aircraft.
UNIT I INTRODUCTION TO AVIONICS 8
Need for Avionics in civil and military aircraft and space systems – Integrated Avionics
system – Typical avionics sub systems – Design approaches and recent advances -
Application Technologies.
UNIT II PRINCIPLES OF DIGITAL SYSTEMS 10
Digital Computers – Digital number system- number systems and codes-Fundamentals
of logic and combinational logic circuits –Digital arithmetic – interfacing with analogue
systems - Microprocessors – Memories.-
UNIT III DIGITAL AVIONICS ARCHITECTURE 8
Avionics system architecture– salient features and applications of Data buses MIL–STD
1553 B–ARINC 429–ARINC 629.
UNIT IV FLIGHT DECK AND COCKPITS 9
Control and display technologies CRT, LED, LCD, EL and plasma panel - Touch screen
- Direct voice input (DVI) - Civil cockpit and military cockpit : MFDS, HUD, MFK, HOTAS
UNIT V AVIONICS SYSTEMS 10
Communication Systems - Navigation systems - Flight control systems - Radar
electronic warfare - Utility systems Reliability and maintainability - Certification.
TOTAL: 45 PERIODS
11
TEXT BOOKS
1. Malcrno A.P. and Leach, D.P., “Digital Principles and Application”, Tata McGraw-Hill,
1990.
2. Gaonkar, R.S., “Microprocessors Architecture – Programming and Application”,
Wiley and Sons Ltd., New Delhi, 1990.
REFERENCES
1. Middleton, D.H., Ed., “Avionics Systems, Longman Scientific and Technical”,
Longman Group UK Ltd., England, 1989.
2. Spitzer, C.R., “Digital Avionic Systems”, Prentice Hall, Englewood Cliffs, N.J., USA.,
1987.
3. Brain Kendal, “Manual of Avionics”, The English Book House, 3rd Edition, New Delhi,
1993.
AE2402 COMPUTATIONAL FLUID DYNAMICS L T P C
OBJECTIVE
To study the flow of dynamic fluids by computational methods
U
NIT I FUNDAMENTAL CONCEPTS 10
Introduction - Basic Equations of Fluid Dynamics - Incompressible In viscid Flows:
Source, vortex and doublet panel, methods - lifting flows over arbitrary bodies.
Mathematical properties of Fluid Dynamics Equations -_ Elliptic, Parabolic and
Hyperbolic equations - Well posed problems - discretization of partial Differential
Equations. Explicit finite difference methods of subsonic, supersonic and viscous flows.
UNIT II GRID GENERATION 7
Structured grids. Types and transformations.Generation of structured grids. Unstructured
grids. Delany triangulation.
UNIT III DISCRETIZATION 8
Boundary layer Equations and methods of solution -Implicit time dependent methods for
inviscid and viscous compressible flows - Concept of numerical dissipation --Stability
properties of explicit and implicit methods - Conservative upwind discretization for
Hyperbolic systems - Further advantages of upwind differencing.
UNIT IV FINITE ELEMENT TECHNIQUES 6
Overview of Finite Element Techniques in Computational Fluid Dynamics. Strong and
Weak Formulations of a Boundary Value Problem.
U
NIT V FINITE VOLUME TECHNIQUES 14
Finite Volume Techniques - Cell Centered Formulation - Lax - Vendoroff Time Stepping -
Runge - Kutta Time Stepping - Multi - stage Time Stepping - Accuracy -. Cell Vertex
Formulation - Multistage Time Stepping - FDM -like Finite Volume Techniques - Central
and Up-wind Type Discretizations - Treatment of Derivatives. Flux – splitting schemes.
Pressure correction solvers – SIMPLE, PESO. Vorticity transport formulation.
Implicit/semi-implicit schemes.
TOTAL: 45 PERIODS
12
TEXT BOOK
1. Fletcher, C.A.J., “Computational Techniques for Fluid Dynamics”, Vols. I and II,
Springer - Verlag, Berlin, 1988.
REFERENCES
1. John F. Wendt (Editor), “Computational Fluid Dynamics - An Introduction”, Springer –
Verlag, Berlin, 1992
2. Charles Hirsch, “Numerical Computation of Internal and External Flows”, Vols. I and
II. John Wiley & Sons, New York, 1988.
3. Klaus A Hoffmann and Steve T. Chiang. “Computational Fluid Dynamics for
Engineers”, Vols. I & II Engineering Education System, P.O. Box 20078, W. Wichita,
K.S., 67208 - 1078 USA, 1993.
4. Anderson, Jr.D., “Fundamentals of Aerodynamics”, McGraw-Hill, 2000.
AE2403 VIBRATIONS & ELEMENTS OF AEROELASTICITY L T P C
OBJECTIVE
To study the dynamic behaviour of different aircraft components and the interaction
among the aerodynamic, elastic and inertia forces
UNIT I BASIC NOTIONS 8
Simple harmonic motion – Terminologies – Newton’s Law – D’ Alembert’s principle –
Energy Methods
UNIT II SINGLE DEGREE OF FREEDOM SYSTEMS 12
Free vibrations – Damped vibrations – Forced Vibrations, with and without damping –
support excitation – Vibration measuring instruments.
UNIT III MULTI DEGREES OF FREEDOM SYSTEMS 10
Two degrees of freedom systems – Static and Dynamic couplings vibration absorber-
Principal co- ordinates, Principal modes and orthogonal condition – Eigen value
problems.
Hamilton’s principle- Lagrangean equation and application – Vibration of elastic bodies-
Vibration of strings- Longitudinal, Lateral and Torsional vibrations.
UNIT IV APPROXIMATE METHODS 5
Rayleigh’s and Holzer Methods to find natural frequencies.
UNIT V ELEMENTS OF AEROELASTICITY 10
Concepts – Coupling – Aero elastic instabilities and their prevention – Basic ideas on
wing divergence, loss and reversal of aileron control – Flutter and its prevention.
TOTAL: 45 PERIODDS
TEXT BOOKS
1. Timoshenko S., “Vibration Problems in Engineering”– John Wiley and Sons, New
York, 1993.
2. Fung Y.C., “An Introduction to the Theory of Aeroelasticity” – John Wiley & Sons,
New York, 1995.
13
REFERENCES
1. Bisplinghoff R.L., Ashley H and Hoffman R.L., “Aeroelasticity” – Addision Wesley
Publication, New York, 1983.
2. Tse. F.S., Morse, I.F., Hinkle, R.T., “Mechanical Vibrations”, – Prentice Hall, New
York, 1984.
3. Scanlan R.H. & Rosenbaum R., “Introduction to the study of Aircraft Vibration &
Flutter”, John Wiley and Sons. New York, 1982.
4. Tongue. B. H., “Principles of Vibration”, Oxford University Press, 2000.
AE2404 AIRCRAFT DESIGN PROJECT – II L T P C
0 0 3 2
OBJECTIVE
• To enhance the knowledge in continuation of the design given in project–I
• Each student is assigned the work in continuation of the design project – I. The
following assignments are to be carried out.
LIST OF EXPERIMENTS
1. V-n diagram for the design study
2. Gust and maneuverability envelopes
3. Critical loading performance and final V-n graph calculation
4. Structural design study – Theory approach
5. Load estimation of wings
6. Load estimation of fuselage.
7. Balancing and Maneuvering loads on tail plane, Aileron and Rudder loads.
8. Detailed structural layouts
9. Design of some components of wings, fuselage
10. Preparation of a detailed design report with drawings.
TOTAL: 60 PERIODS
LIST OF EQUIPMENTS
(for a batch of 30 students)
S.No. Items Quantity
1. Drawing Board 30
2. Drawing Instrument 20
3. Computers and suitable
software
30
AE2405 AIRCRAFT SYSTEMS LABORATORY L T P C
0 0 3 2
OBJECTIVE
To train the students “ON HAND” experience in maintenance of various air frame
systems in aircraft and rectification of common snags.
LIST OF EXPERIMENTS
1. Aircraft “Jacking Up” procedure
2. Aircraft “Levelling” procedure
3. Control System “Rigging check” procedure
4. Aircraft “Symmetry Check” procedure
5. “Flow test” to assess of filter element clogging
14
6. “Pressure Test” To assess hydraulic External/Internal Leakage
7. “Functional Test” to adjust operating pressure
8. “Pressure Test” procedure on fuel system components
9. “Brake Torque Load Test” on wheel brake units
10. Maintenance and rectification of snags in hydraulic and fuel systems.
TOTAL: 60 PERIODS
LIST OF EQUIPMENTS
(for a batch of 30 students)
S.No. Items Quantity Experiment No.
1. Serviceable aircraft with all above
systems
1 1,2,3,4,5,6,7,8,9,10
2. Hydraulic Jacks (Screw Jack) 5 1,2,4,8
3. Trestle adjustable 5 1,2,4,8
4. Spirit Level 2 8
5. Levelling Boards 2 8
6. Cable Tensiometer 1 8
7. Adjustable Spirit Level 1 8
8. Plumb Bob 1 8
AE2406 AVIONICS LABORATORY L T P C
0 0 3 2
OBJECTIVE
This laboratory is divided into three parts to train the students to learn about basic digital
electronics circuits, programming with microprocessors, design and implementation of
data buses in avionics with MIL – Std. 1553B and remote terminal configuration and their
importance in different applications in the field of Avionics.
LIST OF EXPERIMENTS
DIGITAL ELECTRONICS
Addition/Subtraction of binary numbers.
Multiplexer/Demultiplexer Circuits.
Encoder/Decoder Circuits.
Timer Circuits, Shift Registers, Binary Comparator Circuits.
MICROPROCESSORS
Addition and Subtraction of 8-bit and 16-bit numbers.
Sorting of Data in Ascending & Descending order.
Sum of a given series with and without carry.
Greatest in a given series & Multi-byte addition in BCD mode.
Interface programming with 4 digit 7 segment Display & Switches & LED’s.
16 Channel Analog to Digital Converter & Generation of Ramp, Square, Triangular wave
by Digital to Analog Converter.
AVIONICS DATA BUSES
Study of Different Avionics Data Buses.
MIL-Std – 1553 Data Buses Configuration with Message transfer.
MIL-Std – 1553 Remote Terminal Configuration.
TOTAL: 60 PERIODS
15
LIST OF EQUIPMENT
(for a batch of 30 students)
S.No. Details of Equipments Quantity Experiment
Nos.
1. Adder/Subtractor Binary bits Kit 6 1
2 Timer Kit 6 1
3 Encoder Kit 6 3
4 Decoder Kit 6 3
5 Comparator Kit 6 4
6 Multiplexer Kit 6 2
7 Demultiplexer Kit 6 2
8 Shift Registers Kit 6 4
9 Electronic Design Experimeter 6 6,7,9,10
10 Microprocessor 8085 Kit 9 5,6,7,8,9,10
11 4 Digit 7 Segment Display 3 6
12 Switches & LED’s Circuit 3 6
13 16 Channel AD Converter 6 10,9
14 Digital to Analog Converter 6 10
15 Cathode Ray Oscilloscope 3 9,10
16 Regulated Power Supply (5V DC) 9 1, 2,3,4
17 MIL-Std 1553B Setup with Remote
Terminal
1 12,13
18 Computers 2 11,12,13
AE2407 IDENTIFICATION OF PROJECT WORK L T P C
0 0 2 1
OBJECTIVE:
The students shall be divided into convenient groups of not more than 4 members and
will be assigned a staff member as guide. The area and the problem will be identified
along with the problem definition. The students will be initiated into literature survey,
assessment of hard ware and soft ware requirements and initial purchase of materials
and fabrication towards the realization of the project in the ensuing semester
TOTAL: 30 PERIODS
16
SEMESTER VII SEVENTH SEMESTER AERONAUTICAL ENGINEERING ANNA UNIVERSITY CHENNAI SYLLABUS
SEMESTER VII
THEORY
GE2022 Total Quality Management
AE2401 Avionics
AE2402 Computational Fluid Dynamics
AE2403 Vibrations And Elements of Aero elasticity
Elective – II
Elective – III
PRACTICAL
AE2404 Aircraft Design Project - II 0 0 3 2
AE2405 Aircraft Systems Laboratory 0 0 3 2
AE2406 Avionics Laboratory 0 0 3 2
AE2407 Identification of Project Work 0 0 2 1
TOTAL 18 0 11 25
2
GE2022 TOTAL QUALITY MANAGEMENT L T P C
(Common to all branches)
OBJECTIVE
• To understand the Total Quality Management concept and principles and the various
tools available to achieve Total Quality Management.
• To understand the statistical approach for quality control.
• To create an awareness about the ISO and QS certification process and its need for
the industries.
UNIT I INTRODUCTION 9
Definition of Quality, Dimensions of Quality, Quality Planning, Quality costs - Analysis
Techniques for Quality Costs, Basic concepts of Total Quality Management, Historical
Review, Principles of TQM, Leadership – Concepts, Role of Senior Management,
Quality Council, Quality Statements, Strategic Planning, Deming Philosophy, Barriers to
TQM Implementation.
UNIT II TQM PRINCIPLES 9
Customer satisfaction – Customer Perception of Quality, Customer Complaints, Service
Quality, Customer Retention, Employee Involvement – Motivation, Empowerment,
Teams, Recognition and Reward, Performance Appraisal, Benefits, Continuous Process
Improvement – Juran Trilogy, PDSA Cycle, 5S, Kaizen, Supplier Partnership –
Partnering, sourcing, Supplier Selection, Supplier Rating, Relationship Development,
Performance Measures – Basic Concepts, Strategy, Performance Measure.
UNIT III STATISTICAL PROCESS CONTROL (SPC) 9
The seven tools of quality, Statistical Fundamentals – Measures of central Tendency
and Dispersion, Population and Sample, Normal Curve, Control Charts for variables and
attributes, Process capability, Concept of six sigma, New seven Management tools.
UNIT IV TQM TOOLS 9
Benchmarking – Reasons to Benchmark, Benchmarking Process, Quality Function
Deployment (QFD) – House of Quality, QFD Process, Benefits, Taguchi Quality Loss
Function, Total Productive Maintenance (TPM) – Concept, Improvement Needs, FMEA –
Stages of FMEA.
10
UNIT V QUALITY SYSTEMS 9
Need for ISO 9000 and Other Quality Systems, ISO 9000:2000 Quality System –
Elements, Implementation of Quality System, Documentation, Quality Auditing, TS
16949, ISO 14000 – Concept, Requirements and Benefits.
TOTAL: 45 PERIODS
TEXT BOOK
1. Dale H.Besterfiled, et al., “Total Quality Management”, Pearson Education, Inc.
2003. (Indian reprint 2004). ISBN 81-297-0260-6.
REFERENCES
1. Evans. J. R. & Lindsay. W,M “The Management and Control of Quality”, (5th Edition),
South-Western (Thomson Learning), 2002 (ISBN 0-324-06680-5).
2. Feigenbaum.A.V. “Total Quality Management”, McGraw-Hill, 1991.
3. Oakland.J.S. “Total Quality Management”, Butterworth Hcinemann Ltd., Oxford,
1989.
4. Narayana V. and Sreenivasan, N.S. “Quality Management – Concepts and Tasks”,
New Age International 1996.
5. Zeiri. “Total Quality Management for Engineers”, Wood Head Publishers, 1991.
AE2401 AVIONICS L T P C
OBJECTIVE
To introduce the basic concepts of navigation & communication systems of aircraft.
UNIT I INTRODUCTION TO AVIONICS 8
Need for Avionics in civil and military aircraft and space systems – Integrated Avionics
system – Typical avionics sub systems – Design approaches and recent advances -
Application Technologies.
UNIT II PRINCIPLES OF DIGITAL SYSTEMS 10
Digital Computers – Digital number system- number systems and codes-Fundamentals
of logic and combinational logic circuits –Digital arithmetic – interfacing with analogue
systems - Microprocessors – Memories.-
UNIT III DIGITAL AVIONICS ARCHITECTURE 8
Avionics system architecture– salient features and applications of Data buses MIL–STD
1553 B–ARINC 429–ARINC 629.
UNIT IV FLIGHT DECK AND COCKPITS 9
Control and display technologies CRT, LED, LCD, EL and plasma panel - Touch screen
- Direct voice input (DVI) - Civil cockpit and military cockpit : MFDS, HUD, MFK, HOTAS
UNIT V AVIONICS SYSTEMS 10
Communication Systems - Navigation systems - Flight control systems - Radar
electronic warfare - Utility systems Reliability and maintainability - Certification.
TOTAL: 45 PERIODS
11
TEXT BOOKS
1. Malcrno A.P. and Leach, D.P., “Digital Principles and Application”, Tata McGraw-Hill,
1990.
2. Gaonkar, R.S., “Microprocessors Architecture – Programming and Application”,
Wiley and Sons Ltd., New Delhi, 1990.
REFERENCES
1. Middleton, D.H., Ed., “Avionics Systems, Longman Scientific and Technical”,
Longman Group UK Ltd., England, 1989.
2. Spitzer, C.R., “Digital Avionic Systems”, Prentice Hall, Englewood Cliffs, N.J., USA.,
1987.
3. Brain Kendal, “Manual of Avionics”, The English Book House, 3rd Edition, New Delhi,
1993.
AE2402 COMPUTATIONAL FLUID DYNAMICS L T P C
OBJECTIVE
To study the flow of dynamic fluids by computational methods
U
NIT I FUNDAMENTAL CONCEPTS 10
Introduction - Basic Equations of Fluid Dynamics - Incompressible In viscid Flows:
Source, vortex and doublet panel, methods - lifting flows over arbitrary bodies.
Mathematical properties of Fluid Dynamics Equations -_ Elliptic, Parabolic and
Hyperbolic equations - Well posed problems - discretization of partial Differential
Equations. Explicit finite difference methods of subsonic, supersonic and viscous flows.
UNIT II GRID GENERATION 7
Structured grids. Types and transformations.Generation of structured grids. Unstructured
grids. Delany triangulation.
UNIT III DISCRETIZATION 8
Boundary layer Equations and methods of solution -Implicit time dependent methods for
inviscid and viscous compressible flows - Concept of numerical dissipation --Stability
properties of explicit and implicit methods - Conservative upwind discretization for
Hyperbolic systems - Further advantages of upwind differencing.
UNIT IV FINITE ELEMENT TECHNIQUES 6
Overview of Finite Element Techniques in Computational Fluid Dynamics. Strong and
Weak Formulations of a Boundary Value Problem.
U
NIT V FINITE VOLUME TECHNIQUES 14
Finite Volume Techniques - Cell Centered Formulation - Lax - Vendoroff Time Stepping -
Runge - Kutta Time Stepping - Multi - stage Time Stepping - Accuracy -. Cell Vertex
Formulation - Multistage Time Stepping - FDM -like Finite Volume Techniques - Central
and Up-wind Type Discretizations - Treatment of Derivatives. Flux – splitting schemes.
Pressure correction solvers – SIMPLE, PESO. Vorticity transport formulation.
Implicit/semi-implicit schemes.
TOTAL: 45 PERIODS
12
TEXT BOOK
1. Fletcher, C.A.J., “Computational Techniques for Fluid Dynamics”, Vols. I and II,
Springer - Verlag, Berlin, 1988.
REFERENCES
1. John F. Wendt (Editor), “Computational Fluid Dynamics - An Introduction”, Springer –
Verlag, Berlin, 1992
2. Charles Hirsch, “Numerical Computation of Internal and External Flows”, Vols. I and
II. John Wiley & Sons, New York, 1988.
3. Klaus A Hoffmann and Steve T. Chiang. “Computational Fluid Dynamics for
Engineers”, Vols. I & II Engineering Education System, P.O. Box 20078, W. Wichita,
K.S., 67208 - 1078 USA, 1993.
4. Anderson, Jr.D., “Fundamentals of Aerodynamics”, McGraw-Hill, 2000.
AE2403 VIBRATIONS & ELEMENTS OF AEROELASTICITY L T P C
OBJECTIVE
To study the dynamic behaviour of different aircraft components and the interaction
among the aerodynamic, elastic and inertia forces
UNIT I BASIC NOTIONS 8
Simple harmonic motion – Terminologies – Newton’s Law – D’ Alembert’s principle –
Energy Methods
UNIT II SINGLE DEGREE OF FREEDOM SYSTEMS 12
Free vibrations – Damped vibrations – Forced Vibrations, with and without damping –
support excitation – Vibration measuring instruments.
UNIT III MULTI DEGREES OF FREEDOM SYSTEMS 10
Two degrees of freedom systems – Static and Dynamic couplings vibration absorber-
Principal co- ordinates, Principal modes and orthogonal condition – Eigen value
problems.
Hamilton’s principle- Lagrangean equation and application – Vibration of elastic bodies-
Vibration of strings- Longitudinal, Lateral and Torsional vibrations.
UNIT IV APPROXIMATE METHODS 5
Rayleigh’s and Holzer Methods to find natural frequencies.
UNIT V ELEMENTS OF AEROELASTICITY 10
Concepts – Coupling – Aero elastic instabilities and their prevention – Basic ideas on
wing divergence, loss and reversal of aileron control – Flutter and its prevention.
TOTAL: 45 PERIODDS
TEXT BOOKS
1. Timoshenko S., “Vibration Problems in Engineering”– John Wiley and Sons, New
York, 1993.
2. Fung Y.C., “An Introduction to the Theory of Aeroelasticity” – John Wiley & Sons,
New York, 1995.
13
REFERENCES
1. Bisplinghoff R.L., Ashley H and Hoffman R.L., “Aeroelasticity” – Addision Wesley
Publication, New York, 1983.
2. Tse. F.S., Morse, I.F., Hinkle, R.T., “Mechanical Vibrations”, – Prentice Hall, New
York, 1984.
3. Scanlan R.H. & Rosenbaum R., “Introduction to the study of Aircraft Vibration &
Flutter”, John Wiley and Sons. New York, 1982.
4. Tongue. B. H., “Principles of Vibration”, Oxford University Press, 2000.
AE2404 AIRCRAFT DESIGN PROJECT – II L T P C
0 0 3 2
OBJECTIVE
• To enhance the knowledge in continuation of the design given in project–I
• Each student is assigned the work in continuation of the design project – I. The
following assignments are to be carried out.
LIST OF EXPERIMENTS
1. V-n diagram for the design study
2. Gust and maneuverability envelopes
3. Critical loading performance and final V-n graph calculation
4. Structural design study – Theory approach
5. Load estimation of wings
6. Load estimation of fuselage.
7. Balancing and Maneuvering loads on tail plane, Aileron and Rudder loads.
8. Detailed structural layouts
9. Design of some components of wings, fuselage
10. Preparation of a detailed design report with drawings.
TOTAL: 60 PERIODS
LIST OF EQUIPMENTS
(for a batch of 30 students)
S.No. Items Quantity
1. Drawing Board 30
2. Drawing Instrument 20
3. Computers and suitable
software
30
AE2405 AIRCRAFT SYSTEMS LABORATORY L T P C
0 0 3 2
OBJECTIVE
To train the students “ON HAND” experience in maintenance of various air frame
systems in aircraft and rectification of common snags.
LIST OF EXPERIMENTS
1. Aircraft “Jacking Up” procedure
2. Aircraft “Levelling” procedure
3. Control System “Rigging check” procedure
4. Aircraft “Symmetry Check” procedure
5. “Flow test” to assess of filter element clogging
14
6. “Pressure Test” To assess hydraulic External/Internal Leakage
7. “Functional Test” to adjust operating pressure
8. “Pressure Test” procedure on fuel system components
9. “Brake Torque Load Test” on wheel brake units
10. Maintenance and rectification of snags in hydraulic and fuel systems.
TOTAL: 60 PERIODS
LIST OF EQUIPMENTS
(for a batch of 30 students)
S.No. Items Quantity Experiment No.
1. Serviceable aircraft with all above
systems
1 1,2,3,4,5,6,7,8,9,10
2. Hydraulic Jacks (Screw Jack) 5 1,2,4,8
3. Trestle adjustable 5 1,2,4,8
4. Spirit Level 2 8
5. Levelling Boards 2 8
6. Cable Tensiometer 1 8
7. Adjustable Spirit Level 1 8
8. Plumb Bob 1 8
AE2406 AVIONICS LABORATORY L T P C
0 0 3 2
OBJECTIVE
This laboratory is divided into three parts to train the students to learn about basic digital
electronics circuits, programming with microprocessors, design and implementation of
data buses in avionics with MIL – Std. 1553B and remote terminal configuration and their
importance in different applications in the field of Avionics.
LIST OF EXPERIMENTS
DIGITAL ELECTRONICS
Addition/Subtraction of binary numbers.
Multiplexer/Demultiplexer Circuits.
Encoder/Decoder Circuits.
Timer Circuits, Shift Registers, Binary Comparator Circuits.
MICROPROCESSORS
Addition and Subtraction of 8-bit and 16-bit numbers.
Sorting of Data in Ascending & Descending order.
Sum of a given series with and without carry.
Greatest in a given series & Multi-byte addition in BCD mode.
Interface programming with 4 digit 7 segment Display & Switches & LED’s.
16 Channel Analog to Digital Converter & Generation of Ramp, Square, Triangular wave
by Digital to Analog Converter.
AVIONICS DATA BUSES
Study of Different Avionics Data Buses.
MIL-Std – 1553 Data Buses Configuration with Message transfer.
MIL-Std – 1553 Remote Terminal Configuration.
TOTAL: 60 PERIODS
15
LIST OF EQUIPMENT
(for a batch of 30 students)
S.No. Details of Equipments Quantity Experiment
Nos.
1. Adder/Subtractor Binary bits Kit 6 1
2 Timer Kit 6 1
3 Encoder Kit 6 3
4 Decoder Kit 6 3
5 Comparator Kit 6 4
6 Multiplexer Kit 6 2
7 Demultiplexer Kit 6 2
8 Shift Registers Kit 6 4
9 Electronic Design Experimeter 6 6,7,9,10
10 Microprocessor 8085 Kit 9 5,6,7,8,9,10
11 4 Digit 7 Segment Display 3 6
12 Switches & LED’s Circuit 3 6
13 16 Channel AD Converter 6 10,9
14 Digital to Analog Converter 6 10
15 Cathode Ray Oscilloscope 3 9,10
16 Regulated Power Supply (5V DC) 9 1, 2,3,4
17 MIL-Std 1553B Setup with Remote
Terminal
1 12,13
18 Computers 2 11,12,13
AE2407 IDENTIFICATION OF PROJECT WORK L T P C
0 0 2 1
OBJECTIVE:
The students shall be divided into convenient groups of not more than 4 members and
will be assigned a staff member as guide. The area and the problem will be identified
along with the problem definition. The students will be initiated into literature survey,
assessment of hard ware and soft ware requirements and initial purchase of materials
and fabrication towards the realization of the project in the ensuing semester
TOTAL: 30 PERIODS
16
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