airplane performance, stability and control · 9 28 endurance. 29 turning flight performance 30...
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Name of Faculty: AMOL
Discipline: Aeronautical Engineering
Semester:4th
Subject: AIRPLANE PERFORMANCE, STABILITY AND CONTROL
Lesson Plan Duration: 15 weeks (January,2018- Apri,2018)
Week Theory
Lecture Day Topics (including assignment test)
1
1 Atmosphere : ISA
2 Geopotential and Geometric altitude,
3 Troposphere and Stratosphere
4 stability of atmosphere.
2 5 Aerodynamic characteristics : Drag
Aerodynamics
6 Drag polar, estimation of drag
7 Forces and moments from dimensional analysis
3 8 pressure distribution over airfoils
9 variation with angle of attack
10 aerodynamic centre, centre of pressure - related
problems
4 11 variation of aerodynamic coefficients with
Reynolds number and Mach number
12 Effect of span, aspect ratio, planform, sweep
13 taper and twist on aerodynamic characteristics.
5 14 High lift devices
15 V/STOL configurations
16 Airplane Performance in Steady and Level
Flight : Equations of motion of aircraft,
17 variation of drag with flight, power required
6 18 variation of drag with power available
19 minimum drag
20 minimum power conditions
7 21 climbing performance
22 gliding performance
23 Airplane Performance in Accelerated Flight:
Take off
8 24 landing distances
25 Jet Assisted
26 Take off
27 Range
9 28 Endurance.
29 Turning flight performance
30 Static longitudinal stability : Stick fixed static
longitudinal stability
31 neutral point, power effects,
10 32 stick free static longitudinal stability.
33 Hinge moments, Aerodynamic Balancing,
Static Margin. In flight measurement of stick
fixed and stick free neutral points. maneuver
margin.
34 Maneuvering flight : Elevator angle per g and
stick force per g maneuver margin.
11 35 Lateral and Directional Stability and Control: Assymmetric flight, weather cock stability,
36 Rudder fixed and Rudder free static directional
stability
37 Rudder lock, dihedral effect.
12 38 Control in Roll, Aileron control power. Cross
coupling of lateral and directional effects. Numerical problem
39 Dynamic Stability : Equations motion of
airplane,
40 stability derivatives
13 41 split-up of equations in symmetrical
42 non-symmetric groups of motion.
43 Analysis of short period.
14 44 phugoid
45 Analysis of roll modes
46 Analysis of spiral modes
15 47 Dutch Roll.
48
Name of Faculty: AMOL
Discipline: Aeronautical Engineering
Semester: 6th
Subject: AIRCRAFT MATERIALS
Lesson Plan Duration: 15 weeks (January,2018- Apri,2018)
Week Theory
Lecture Day Topics (including assignment test)
1
1 Engineering Materials, Structural properties of
materials
2 Atomic and lattice structure,
3 bonding in Solids
4 Imperfections in crystals
2 5 Solid phase and phase diagrams
6 mechanical properties and testing,
7 Isotropy, Orthotropy
3 8 True stress and strain
9 Strength and elasticity
10 Stiffness, Resistance, Plasticity, Ductility,
Toughness and Hardness of materials.
4 11 Concept of Fatigue and Creep,
12 Mechanical Testing,
13 Factors Affecting Strength, Deformation, Plasticity
and Viscoelasticity, Fracture, Heat treatment
5 14 Chemical, thermal and Technological Properties,
15 Board classification of aircraft materials
16 Ferrous materials, nonferrous materials and alloys
17 ceramic materials and fibre reinforced
composite materials, polymers, metal matrix
particulate.
6 18 Furnishing Materials
19 Plastic, wood, plywood
20 glue, dopes and rubber used in aircraft manufacture
7 21 Methods of testing
22 Methods of storage,
23 Paints, surface finishes and materials
8 24 Specifications: Indian Standard
25 British, American, French,
26 German, and International specifications
27 Corrosion, its detection and prevention
9 28 Protective finishes
29 Testing
30 Destructive techniques.
31 non - destructive testing techniques.
10 32 Crack detection
33 inspection of parts by hot oil
34 inspection of parts by chalk
11 35 dye-penetrant,
36 Fluorescent particles
37 magnetic particles
12 38 X-ray
39 ultrasonic
40 eddy current.
13 41 acoustic emission methods.
42
43
14 44
45
46
15 47
48
Name of Faculty: AMOL
Discipline: Aeronautical Engineering
Semester: 4th
Subject: MAINTENANCE OF RADIO & COMMUNICATION SYSTEMS
Lesson Plan Duration: 15 weeks (January,2018- Apri,2018)
Week Theory
Lecture Day Topics (including assignment test)
1
1 Basics of the application and identification of electrical cables used in Aircraft radio installation
2 crimping and soldering techniques
3 bonding continuity and insulation tests.
4 Composition
2 5 performance (stability and tolerance
6 limitations of the fixed resistors
7 limitations of the varistors (carbon composition, carbon film, wire wound and metallic film).
3 8 AC and DC measuring instruments:
9 Electrical power distribution systems
10 the operation and construction of static
4 11 the operation and construction of inverters,
12 the operation and construction of static rotary inverters
13 the operation and construction of transformer rectifier units.
5 14 AC and DC measuring instruments: Electrical power distribution systems, the operation and construction of static inverters, rotary inverters and transformer rectifier units. Basics of interference caused by electrical and
ignition system to radio apparatus, methods of
minimizing or suppressing such interference,
bonding and screening
15 Basics of interference caused by electrical and
ignition system to radio apparatus
16 methods of minimizing or suppressing such
interference
17 bonding and screening
6 18 Construction and Identification of various types of antennas
19 the voltage and current distribution along antenna of various length
20 characteristics of ground planes.
7 21 Very high frequency (VHF)
22 high frequency (HF)
23 airborne communications
8 24 frequency bands allocation
25 methods of propagation
26 ranges expected both day and night
27 calculation of approximate range of communication (line of sight) with given data.
9 28 The performance levels
29 specifications of typical airborne
30 VHF communication systems
31 the principle of operation
10 32 installation practices
33 functioning of the operating controls
34 maintenance of typical HF and VHF communication transceivers.
11 35 Theory of operation
36 performance level
37 specifications of an Audio Integration System
12 38 Working principles and testing of Lead Acid batteries Principles,
39 Working principles and testing of Nickel Cadmium and Silver Zinc batteries Principles,
40 Principles, Characteristics and operation of the under mentioned systems:
13 41 Automatic Direction Finder (ADF) Systems, Very High Frequency (VHF) Omn
42 Directional Range System
43 Instrument Landing Systems,
14 44 Weather Radar Systems,
45 Omega Navigation System
46 Radio Altimeter Systems, ‡ Cockpit Voice Recorder, Principles of Satellite Communications and its application to aircraft.
15 47 Cockpit Voice Recorder
48 Principles of Satellite Communications and its application to aircraft.
Name of Faculty: AMOL
Discipline: Aeronautical Engineering
Semester: 4th
Subject: AIRCRAFT INSTRUMENTATION
Lesson Plan Duration: 15 weeks (January,2018- Apri,2018)
Week Theory
Lecture Day Topics (including assignment test)
1
1 Measurement of circuit Units and Standards,
2 theory of measurement
3 functional analysis of measurements,
4 errors and error estimation
2 5 Measurement of voltage and current in DC and
AC
6 VTVM digital voltmeter
7 measurement of power
3 8 phase angle, power factor, Extension of range
by instrument transformers,
9 fluxmeter, measurement of frequency,
10 heterodyne techniques s
4 11 digital frequency counters, signal generator
12 LCR direct and bridge methods,
13 Waveform analysis,
5 14 Cathode ray oscilloscopes
15 measurement of harmonic and Intermodulation
distortion
16 distortion analyser, spectrum
17 lanalyser, configurations and performance
characteristics of instruments,
6 18 motion requirement, relative displacement and velocity,
19 Translational and sesmic displacement,
20 velocity and acceleration measurements,
7 21 Very high frequency (VHF)
22 Torque measurement and rotating shaft, pressure and flow
23 temperature based on expansion, electric resistance and radiation methods, Problems
involved in temperature measurements, compensation technique
8 24 Electrostatic Sensitive Devices,
25 Electromagnetic Environment Requirements
for airborne equipment,
26 sensors for the measurement of altitude, air
speed
27 acceleration, temperature, fuel flow and
quantity. Instrument displays,
9 28 The performance levels
29 Moving map display
30 multifunction displays
31 head-up displays
10 32 glass cockpit
33 Cockpit lighting
34 panels: integral,
11 35 glopanels,
36 Typical Electronic/
37 Digital Aircraft Systems:
12 38 ECAM, (Electronic Centralised Aircraft
Monitoring),
39 EFIS (Electronic Flight InstrumentSystems), ,
40 EICAS (Engine Indicating & Crew Alerting
Systems
13 41 FMS (Flight Management Systems)
42 Directional Range System
43 Instrument Landing Systems,
14 44 Weather Radar Systems,
45 Omega Navigation System
46 Radio Altimeter Systems, ‡ Cockpit Voice Recorder, Principles of Satellite Communications and its application to aircraft.
15 47 Cockpit Voice Recorder
48 Principles of Satellite Communications and its application to aircraft.
Name of Faculty: AMOL
Discipline: Aeronautical Engineering
Semester: 6th
Subject: AIRCRAFT PRODUCTION
Lesson Plan Duration: 15 weeks (January,2018- Apri,2018)
Week Theory
Lecture Day Topics (including assignment test)
1
1 Introduction: Function of process planning
(Methods)
2 Organizing for process planning
3 production planning and control
4 Relationship with other departments
2 5 Tool engineering.
6 Heat Treatment
7 Final and intermediary heat treatment operations
carried out on aircraft materials (both ferrous and
non-ferrous
3 8 the equipment used,
9 the importance of test pieces
10 Finishing by anodizing
4 11 General activities
12 carried out in manufacturing
13 assembly shops
5 14 machine shop
15 sheet metal shop
16 welding shop
17 plastic shop
6 18 assembly shop
19 Jigs and Fixtures: Importance of special
production tools used in manufacturing activity of
various types of jigs and fixtures used in aircraft
industry
20 Difference between jigs and fixtures.
7 21 Design consideration
22 Choice of materials
23 Types of assembly fixtures such as table box
8 24 picture-frame, next and so on
25 Typical jigs for wings,
26 fuselage and control surfaces
27 jigs and fixtures for turning, milling and drilling
9 28 Universal tooling
29 Cutting Tools: Theory of metal cutting
30 typical types of cutting tools used in the
manufacturing shops
31 the advantages of tipped tools. Ceramic tools, tool
life, optimum cutting speeds and feeds
10 32 factors limiting speeds, feeds and cuts
33 New development in cutting tools, use of DBN
Diamond
34 ceramics and coating on cutting tools
11 35 Inspection Gauges and Equipment
36 Various inspection gauges in the manufacturing
shops and their application
37 Fits, limits and tolerances, engineering reference
systems,
12 38 station and datum lines, chord and fuselage
reference lines
39 lofting aerofoil, use of templates, test equipment
used in aircraft production, necessity for and
importance of interchangeability media
40 application of inter -change-ability media viz.,
acceptance gauge
13 41 reference gauges, aperture gauges. Use of digital
read out on measuring tools
42 Process Planning : Definition of mass and batch production
43 various types of charting techniques viz., operation
process chart,
14 44 flow process chart etc., definition of planning
breakdown and its importance
45 factors to be considered for process planning,
comparison of methods, simple exercise on process
planning
46 simple machine shop and sheet metal components
15 47 Different approaches in process planning during pre-production and production phases.
48 Process Shop: Theory of planting, finishing processes carried on aircraft materials - planting and finishing equipment
Name of Faculty: AMOL
Discipline: Aeronautical Engineering
Semester: 6th
Subject: wind tunnel technique
Lesson Plan Duration: 15 weeks (January,2018- Apri,2018)
Week Theory
Lecture Day Topics (including assignment test)
1
1 Wind Tunnel as a Tool: Types of wind tunnels,
2 special purpose wind tunnels
3 Wind Tunnel Design: Test section
4 diffuser
2 5 fan section
6 fan design
7 , return passage
3 8 cooling,
9 the breather- vibration
10 test section flow quality
4 11 , diffuser design,
12 wind tunnel construction
13 , energy rat
5 14 , final form
15 Instrumentation and Calibration of Test Section:
Measurement of pressure
16 velocity, turbulence
17 , flow angularity
6 18 , hot wire anemometry,
19 laser velocimeter
20 , data acquisition
7 21 flow visualizatio
22 , wind tunnel calibration
23 Model Forces, Moment and Pressure
Measurement
8 24 Wind tunnel balances
25 - Internal & External balances design of wind
tunnel balances
26 , Wake survey method
27 Wind Tunnel Correction: Method of Images
9 28 , boundary corrections
29 , buoyancy corrections
30 wake blockage
31 solid blockage- (2D & 3D corrections
10 32 Non Aeronautical Uses of the Wind Tunnel
33 Applications in wind engineering
34 Surface vehicle testing
11 35 testing of buildings for wind force
36 , pollution,
37 other application
12 38 , other applications at low Reynolds numbers
39
40
13 41
42
43
14 44
45
46
15 47
48
Name of Faculty: AMOL
Discipline: Aeronautical Engineering
Semester: 6th
Subject: NON DESTRUCTIVE EVALUATION
Lesson Plan Duration: 15 weeks (January,2018- Apri,2018)
Week Theory
Lecture Day Topics (including assignment test)
1
1 Importance of NDT in quality assurance
2 Different types of non destructive techniques to
obtain information regarding siz
3 location of damage or cracks
4 orientation of damage or cracks
2 5 Visual inspection techniques
6 coin tapping technique for composite structures
7 adhesive bonds.
3 8 Ultrasonic testing
9 Pulse echo technique
10 pitch-catch technique
4 11 through transmission technique
12 A-scan
13 B-Scan
5 14 C-scan
15 Acoustic emission
16 Sources of acoustic emission in composites
17 peak amplitude
6 18 rise time during event
19 ring-down counts duration of events
20 X-ray radiography
7 21 Absorption spectra
22 short wave length,
23 X-ray for detection of voids
8 24 Die penetration technique
25 Magnetic particle testing
26 In each of the above techniques, (i) theory
27 In each of the above techniques, (i) theory basic
principles,
9 28 advantages
29 disadvantages,
30 (ii) material of parts that can be inspected
31 (iv) physical size
10 32 shape limitation
33 economics of process
34 types of defects that can be detected
11 35 environment limitation are to be discussed alongwith equipment used for each of the techniques.
36
37
12 38
39
40
13 41
42
43
14 44
45
46
15 47
48
Name of Faculty: AMOL
Discipline: Aeronautical Engineering
Semester: 6th
Subject: Aircraft propulsion-II
Lesson Plan Duration: 15 weeks (January,2018- Apri,2018)
Week Theory
Lecture Day Topics (including assignment test)
1
1 Steady 1-D Gas Dynamics: Basics
2 Simple flows; Nozzle flow
3 nozzle design, nozzle operating
4 nozzle flow and shock waves
2 5 Nozzle characteristics of some operational Engines
6 Rayleigh flow and Fanno flow
7 Inlet: design, sizing
3 8 performance for various flow regimes
9 Nozzle: C-D Nozzle performance
10 Effects of back pressure
4 11 exit area ratio and mass flow Combustion Systems
12 Basics of combustion chamber
13 Ignition system
5 14 Flame stability and after burners.
15 basic assumptions
16 Applications to (i) Ramjet
17 (ii) Turbojet with and without after burner
6 18 (iii) Turbo fan Engine, optimum by pass ratio
19 (iv) Turbo-Prop Engine Cycle analysis of real engines
20 Axial Flow Compressor: Euler's Turbo-machinery
equations
7 21 Axial Flow analysis
22 Velocity diagrams
23 flow annulus area stage parameters
8 24 Degree of reaction
25 cascade airfoil nomenclature
26 loss coefficient
27 and flow coefficient, stage pressure ratio
9 28 Blade Mach no
29 Repeating-stage, Repeating-row
30 Meanline design. Flow path dimensions
31 number of blades per stage
10 32 Radial variation
33 Design Process, Performance
34 Axial Flow Turbine : Introduction to turbine
analysis
11 35 mean-radius stage calculations
36 Stage parameters
37 stage loading and flow coefficients
12 38 degree of reaction
39 Stage temperature ratio and pressure ratio
40 Rocket-sled facility
13 41 Eddy current based displacement probe
42 Bending critical speed of simple shaft
43 Blade spacing
14 44 Radial Variation,
45 Velocity ratio. Axial Flow Turbine stage Flow path
dimension
46 stage analysis
15 47 Multistage design steps of design - single stage and
two - stage
48 Turbine Performance, Blade Cooling
Name of Faculty: AMOL
Discipline: Aeronautical Engineering
Semester: 6th
Subject: AIRCRAFT STRUCTURES – II
Lesson Plan Duration: 15 weeks (January,2018- Apri,2018)
Week Theory
Lecture Day Topics (including assignment test)
1
1 Bending of thin plates
2 pure bending
3 plate subjected to bendin
4 plate subjected to twisting
2 5 plates subjected to distributed load,
6 combined bending and in-plane loading of a thin
rectangular plate
7 energy method for bending of thin plates
3 8 STRUCTURAL STABILITY
9 Euler buckling of columns
10 inelastic stability of columns
4 11 effect of initial imperfections
12 energy method for the calculation of buckling loads
in columns
13 flexural and torsional buckling of the thin walled
columns
5 14 buckling of stiffenced plates
15 local instability
16 Stress analysis of aircraft components
17 tapered beams,
6 18 fuselages
19 wings
20 fuselage frames,
7 21 wing ribs
22 shear lag.
23 Matrix methods of structural analysis
8 24 stiffness matrix for an elastic springs,
25 pin jointed frame work
26 application to statically indeterminate frame works
27 matrix analysis of space frames
9 28 stiffness matrix for a beam
29 Concept and introduction to finite element methods
30 Introduction to vibration
31 Free vibration of single
10 32 forced vibration of single
33 two degrees of freedom systems
34 multiple degrees of freedom systems
11 35 Principal modes
36 normal modes
37 static coupling
12 38 dynamic coupling.
39
40
13 41
42
43
14 44
45
46
15 47
48
Name of Faculty: AMOL
Discipline: Aeronautical Engineering
Semester: 8th
Subject :Gas dynamics
Lesson Plan Duration: 15 weeks (January,2018- Apri,2018)
Week Theory
Lecture Day Topics (including assignment test)
1
1 Normal Shock Waves : Equation of motion for a
normal shock
2 normal shock relations for a perfect gas
3 stagnation conditions
4 Rankine-Hugoniot relations
2 5 Propagating shock waves
6 weak shock
7 Reflected shock wave
3 8 centered expansion waves
9 shock tube.
10 Oblique Shock Waves : Introduction
4 11 oblique shock relations
12 relation between shock angle
13 turning angle,
5 14 oblique shock chart
15 Supersonic flow over a wedge, weak oblique shock
16 Boost glide trajectory
17 Expansion Waves: Supersonic expansion by
turning
6 18 Prandtl-Meyer flow
19 Simple and non-simple regions
20 Reflection and interaction of shocks and expansion
waves
7 21 Mach reflection
22 method of characteristics
23 Airfoils in Compressible Flow : Introduction:
Linearized compressible flow
8 24 Airfoils in subsonic flow
25 Prandtl-Glauert transformation
26 critical Mach number, supercritical flow
27 Governing equation,
9 28 Shock wave-boundary layer interaction, stability and control problems.
29 Lift and drag in supersonic flow: Shock
expansion theory
30 Flow field in supersonic flow
31 Thin airfoil theory
10 32 Analytical determination of lift, drag coefficients
on flat plate
33 bi- convex, diamond -shaped profiles in supersonic
flow
34 supersonic flow past wings
11 35 Potential equation for compressible flows:
Introduction
36 Damping in Roll.
37 Manoeuvring Flight: Introduction, Flat turns for
cruciform and monowing
12 38 linearization of potential equation
39 boundary conditions.
40 Small perturbation theory
13 41 application to wavy wall and bodies of revolution
42 Measurements in compressible flows: Instruments used in compressible flow
43 Rayleigh - Pitot-formula,
14 44 Subsonic, transonic and supersonic wind tunnels-
Design and operation of supersonic wind tunnel.
45 Flow visualization by interferometer, schlieren and
shadow graph methods
46 Instrumentation for Hypersonic wind and shock
tunnels
15 47 Aeroballistic range,
48 Terminal ballistic range. Rocket-sled facility
Name of Faculty: AMOL
Discipline: Aeronautical Engineering
Semester: 8th
Subject: Rocket and missiles
Lesson Plan Duration: 15 weeks (January,2018- Apri,2018)
Week Theory
Lecture Day Topics (including assignment test)
1
1 General Introduction : Difference between
Rockets and Missiles
2 Types of Rockets
3 Types of Missiles
4 Satellite launch vehicles
2 5 Manned Rockets
6 Aerodynamics Characteristics of Air Frame
Components
7 Introduction,
3 8 Bodies of revolution
9 Different forebody shapes
10 Base pressure
4 11 Aerodynamic controls
12 Jet control.
13 Performance of Missiles and Rockets
5 14 Introduction
15 various types of drags
16 Boost glide trajectory
17 Graphical solution
6 18 Boost sustainer trajectory
19 long range cruise trajectory
20 long range Ballistic trajectory
7 21 Powered and unpowered flight. Brief description of
Fin stabilized
22 spin stabilized rockets and their force systems
23 Thrust misalignment
8 24 Stability and Control
25 Longitudinal: Two degrees of freedom analysis
26 complete missile aerodynamics with forward and
rear control
27 Static stability margin
9 28 Directional: Introduction
29 cruciform configuratio
30 Body contribution on directional control
31 Wind contribution on directional control
10 32 Tail contribution on directional control
33 Lateral: Induced Roll
34 Interal control and design consideration for
cruciform
11 35 monowing
36 Damping in Roll.
37 Manoeuvring Flight: Introduction, Flat turns for
cruciform and monowing
12 38 Pull ups Relationship of manoeuvrability
39 static stability margin
40 Dynamic Stability : Equations of motion
13 41 longitudinal and lateral dynamics
42 Miscellaneous : Launching problems
43 Re-entry
14 44 Modern Concepts
45 Manned Missions
46 stage analysis
15 47 Multistage design steps of design - single stage and
two - stage
48 Turbine Performance, Blade Cooling