ACS COLLEGE OF ENGINEERINGDEPARTMENT OF AERONAUTICAL ENGINEERING SCHEME AND SYLLABUS FROM ACADEMIC YEAR 2010-11 V SEMESTER Sl No 1 Subject Code 10AL51 Title Management and Entrepreneurship Introduction to Composite Materials Teachin g Dept. Teaching Hours / week Examination Th. Pr. Durat ion I.A Marks Theory/ Practical Total Marks @ 04 -- 03 25 100 125 AE/ME 04 -- 03 25 100 125 AE/ME 04 -- 03 25 100 125 AE 04 -- 03 25 100 125 2 10AE52 3 10AE53 4 10AE54 Dynamics of Machines Aerodynamics – I 5 10AE55 Aircraft Propulsion AE 04 -- 03 25 100 125 6 10AE56 Aircraft Structures – I AE 04 -- 03 25 100 125 7 10AEL57 Aerodynamics Lab Energy Conversion 10AEL58 Lab AE -- 03 03 25 50 75 AE/ME -- 03 03 25 50 75 24 09 24 200 700 Note: One question has to be set for every unit (6 to 8 hours of teaching). @ - Indicates that teaching department can be any Engineering Department / Department of Management Studies 900 8 Total Scheme of examination: One Question to be set from each unit. Students have to answer any FIVE full questions out of EIGHT questions, choosing at least 2 questions from part A and 2 questions from part B. Department of Aeronautical Engineering, ACSCE 1 Motivation Theories. Levels of Management. Development of Entrepreneurship. Small Business Enterprises .Pearson Education/PHI .Departmentation Committees. 6 Hrs UNIT . KSSIDC.Robers Lusier . Types of Help. Skill Development .N. Project Appraisal.4 Directing & Controlling: Meaning and nature of directing Leadership styles.Management & Entrepreneurship Sub Code: Hrs/ Week: Total Hours: 10AL51 04 52 IA Marks: Exam Hours: Exam Marks: PART – A: 25 03 100 Management UNIT .S. Errors of Project Report.17th Edition. M.its Barriers. C. Reference books: 1 Management Fundamentals .Management as a science. 2003. DIC Single Window Agency.2006 (2 & 4).Concepts. Class. TECKSOK. KSIMC.2 Planning: Nature.Management & Administration .Thomson 2 Entrepreneurship Development .nature and characteristics of Management. Types of Entrepreneur. Technical Feasibility Study. Characteristics. Need and rationale.8 Preparation Of Project: Meaning of Project. SISI. Role of entrepreneurs in Economic Development. Scope and Functional areas of management . Entrepreneur – an emerging. Different Policies of SSI.Pearson Edn .coordination.3 Organizing And Staffing: Nature and purpose of organization Principles of organization .Roles of Management. KSFC. Project Identification.Khanka .S. Contents. Ancillary Industry and Tiny Industry (Definition Only) 7 Hrs UNIT . Formulation.Types of plans (Meaning Only) Decision making Importance of planning . Government Support for SSI during 5 year plans. Project Report. Stages in entrepreneurial process.1 Management: Introduction .5 Entrepreneur: Meaning of Entrepreneur. NSIC. meaning and importance and Techniques of Co Ordination. Guidelines by Planning Commission for Project report. Meaning and steps in controlling . Entrepreneurship in India.Tripathi.Essentials of a sound control system .7 Institutional Support: Different Schemes. Impact of Liberalization. Financial Feasibility Study & Social Feasibility Study. importance and purpose of planning process Objectives . art of profession .Stephen Robbins .Meaning . role of SSI in Economic Development. Globalization on SSI Effect of WTO/GATT Supporting Agencies of Government for SSI. Objectives.S.the Concept.Chand & Co. 3 Management .Centralization Vs Decentralization of authority and responsibility Span of control .Government policy towards SSI.Evolution of Entrepreneurship. Need and Significance of Report. 7 Hrs Text books: 1 Principles of Management – P. Evolution of . 6 Hrs UNIT . Department of Aeronautical Engineering.Meaning and importance . Application. ACSCE 2 . Concept of Entrepreneurship . Meaning.Types of organization . Network Analysis. Development of Management Thought .early management approaches – Modern management approaches. 6 Hrs UNIT – 6 Small Scale Industries: Definition. 6 Hrs UNIT . P. Entrepreneurship . Communication .steps in planning & planning premises . Project Selection. Functions of an Entrepreneur. 2 Dynamics of Entrepreneurial Development & Management Vasant Desai .Himalaya Publishing House 3 Entrepreneurship Development – Poornima. KIADB.Methods of establishing control (in brief): 7 Hrs PART-B: Entrepreneurship UNIT . Reddy – Tata McGraw Hill. Advantages of SSI Steps to start and SSI . Identification of business opportunities: Market Feasibility Study.MBO and MBE (Meaning Only) Nature and importance of staffing-:Process of Selection & Recruitment (in brief).Hierarchy of plans. 7 Hrs UNIT . Scope. SIDBI. Functions. Nature of support. Privatization. Objectives. 9th edition. "Composite materials hand book". Forming Metal handbook. blow molding. marine. future potential of composites. 06 Hrs Fabrication Of Composite Structures: Cutting. PART B Unit 5. injection molding. 06 Hrs Macro-Mechanical Behavior of a Laminate: Classical plate theory. computer-aided design and manufacturing. thermo . Aircrafts. injection. 2nd Edition. mechanical fasteners and adhesive bonding. Meing Schwaitz. 3. liquid molding. classification and characteristics of composite materials – fibrous composites. 1975 Reference: 1. micro-mechanics based analysis and experimental determination of material constants. Cambridge University Press. laminated.Stress and strain variation in a laminateResultant forces and moments. Application ofMMC’s. drilling. 4. Unit 4. Text Books: 1. transformation of coordinates. Automobile. production procedures for bag molding. P327 338.Introduction to Composite Materials Sub Code: Hrs/ Week: Total Hours: 10AE52 04 52 IA Marks: Exam Hours: Exam Marks: 25 03 100 PART A Unit 1. 1998 2. Composites Science and Engineering. 08 Hrs Metal Matrix Composites: Reinforcement materials. recreational and Sports equipment. 1990. missiles. machining. 06 Hrs Macro-Mechanical Behavior of a Lamina: Stress-strain relation for an orthotropic lamina.K Chawla. joining. Matrix materials Unit 2. Electrical and electronics. ASM handbook. ACSCE 3 . New York. 2002.open and closed mould process hand layup techniques structural laminate bag molding. Department of Aeronautical Engineering. 1988.Strength analysis of a laminate Unit 8. Hull and Clyne. tooling. McGraw Hill Book Company. Unit 6. pultrusion. Introduction to Composite materials. pulforming. K. Unit 7. V15. McGraw-Hill. Springer Verlag. Mechanics of composites by Artar Kaw.A B & D matrices.Restriction on elastic constants-Strengths of an orthotropic lamina and Failure theories for an orthotropic lamina. R M Jones. 08 Hrs Advanced Processing Techniquesand Application Of Composites: Filament winding. Unit 3. characteristics and selection of base metals. types. 06 Hrs Introduction To Composite Materials: Definition. fabrication equipment.forming. 1984 2. fabricating process . “ Mechanics of Composite Materials”. Space hardware. 06 Hrs Micro-Mechanical Behavior of a Lamina: Determination of elastic constants-Rule of mixtures. 06 Hrs Fiber Reinforced Plastic Processing: Layup and curing. CRC Press. 2006. Effect of gyroscopic couple on ship. Theory of Machines by Thomas Bevan. Text Books: 1. V-type engine. Balancing of several rotating masses by balancing masses in same plane and in different planes. Department of Aeronautical Engineering. Unit 4. Static force analysis of four bar mechanism and slider-crank mechanism with and without friction. 08 Hrs Balancing of Reciprocating Masses: Inertia effect of crank and connecting rod. Srinivas. Radial engine – Direct and reverse crank method. sensitiveness. Murthy. 06 Hrs Dynamic Force Analysis: D’Alembert’s principle. Norton. 2007. New Delhi. Controlling force. Unit 3. 2002. stability. Design of Machinery by Robert L. ratio of belt tensions. Turning moment diagrams and flywheels. 06 Hrs Governors: Types of governors. Belt drives: Flat belt drives. S. L. Dynamics of machinery by J. McGraw Hill.Dynamics of Machinery Sub Code: Hrs/ Week: Total Hours: 10AE53 04 52 IA Marks: Exam Hours: Exam Marks: 25 03 100 PART-A Unit 1. Tata McGraw Hill Ltd. centrifugal tension. force analysis of Porter and Hartnell governors. Undercutting in Cams. Members with two forces and torque. principle of virtual work. 3. 4. ACSCE 4 . 08 Hrs Friction and Belt Drives: Definitions: Types of friction: laws of friction. 2.. plane disc. balancing in multi cylinder-inline engine primary & Secondary forces. Inertia force. Pearson Education. Balancing of single rotating mass by balancing masses in same plane and in different planes. Das & P. 06 Hrs Balancing of Rotating Masses: Static and dynamic balancing. Theory of Machines: Sadhu Singh. 06 Hrs Analysis of CAMS: Analysis of Tangent cam with roller follower and Circular arc cam operating flat faced and roller followers. stability of two wheelers and four wheelers. 2001. Unit 8. 2nd edition. CBS Publication 1984.S. 2nd Edn. Mechanisms and Dynamics of Machinery by J. Dynamic force analysis of fourbar mechanism and slider crank mechanism. 2. Unit 2. Unit 6. single cylinder engine. Chennai. Friction in pivot and collar bearings. Fluctuation of Energy. B. PART-B Unit 5. Reference: 1. K. 06 Hrs Gyroscope: Vectorial representation of angular motion. Scitech Publications. isochronism. effort and power Unit 7. Gyroscopic couple. Dynamically equivalent systems. inertia torque. Equilibrium of two and three force members. power transmitted. Theory of Machines: Rattan S. Determination of size of flywheels. Free body diagrams. aeroplane. 06 Hrs Static Force Analysis: Static force analysis: Introduction: Static equilibrium. Governing equations for irrotational. 06 Hrs Incompressible Flow Over Airfoils Kelvin’s circulation theorem and the starting vortex. J. J J. Anderson. non-lifting flow over a two-dimensional circular cylinder and vortex flow. Edward Arnold Printers Ltd. New York. ”Mechanics of Fluids”. D’Alembert’s paradox. KL. 1966 2. calculation of airfoil lift and drag from measured surface pressure distributions. 06 Hrs Introduction to Viscous Flows Navier-Stokes equations. New York. pathlines. viscous flow over two-dimensional streamlined and bluff bodies and drag characteristics. incompressible flow. 2004 4. Pressure and Aerodynamic load measurements on a model. Classical thin airfoil theory for symmetric and cambered airfoils.B Unit 5. (Special Indian Edition)..”Low Speed Wind Tunnel testing”. 1965 Department of Aeronautical Engineering. “High Speed Wind Tunnel Testing”. (4th Edition). Unit 6. John Wiley & Sons Inc. and Harper. Pope A. 3. Jr. New York. ACSCE 5 . Unit 8. Houghton E. 10 Hrs PART . Anderson. centre of pressure. 5. “Aerodynamics for Engg. aspects of boundary layer separation and airfoil stall. pitot-tube measurement of airspeed. inviscid and viscous flows. Tata McGraw-Hill. Laplace equation and boundary conditions. References : 1. condition on velocity for incompressible flow. Description of Fluid Motion Euler and Lagrangian descriptions. 08 Hrs Introduction to Aerodynamic Testing Principles of wind tunnel flow simulation. and Goin. 6 Hrs Airfoil Characteristics Fundamental aerodynamic variables. compressibility. 6 Hrs Unit 3. Review of Basic Fluid Mechanics Continuity. 2. Lifting flow over a two-dimensionalcircular cylinder. Mach number regimes. CBS Publications1993. John Wiley Inc. displacement. Two-Dimensional Inviscid Incompressible Flows Bernoulli’s equation. momentum and energy equation. vorticity. “Fundamentals of Aerodynamics”. pressure coefficient. Eulers equations of motion. Pope A. boundary layer concept.D. Kutta-Joukowski theorem and generation of lift. circulation. vortex sheet. “Boundary Layer Theory” Mc Graw Hill. open and closed circuit wind tunnels. 4 Hrs Unit 2.Aerodynamics – I Sub Code: Hrs/ Week: Total Hours: 10AE54 04 52 IA Marks: Exam Hours: Exam Marks: 25 03 100 PART – A Unit 1. Duncan WJ. New Delhi. Unit 7. streamlines and streaklines.W.D. Thom AS and Young AD. and Major features of low speed. angular velocity. typical airfoil aerodynamic characteristics at low speeds. Two-dimensional source. momentum thickness and wall skin friction. 2 Edn. Text Books 1. 06 Hrs Flow Over Circular Cylinders Non-lifting flow over a two-dimensional circular cylinder. 2007. smoke and tuft flow visualization techniques. 2007. Jr. aerodynamic forces and moments. control volume approach to continuity and momentum equations. H. J. Schlichting. Tata McGraw-Hill.L and Carpenter P. transonic and supersonic wind tunnels. total drag determination of two-dimensional bodies using wake survey at low speeds. Kutta condition. sink and doublet flows. airfoil section geometry and wing planform geometry.. units and dimensions. “Introduction to Flight”. Students. stream function. Unit 4. velocity potential and relationship between them. . Unit 2. “ Gas Turbine”. & Peterson. Unit 6.L. Basics of heat transfer. Standard Publishers & Distributors. Heat & mass transfer by Domkundwar Department of Aeronautical Engineering.F. 07 Hrs Intoduction to Turbines: Types of turbines-Operating Priciple-Design consideration – Velocity triangles – degree of reaction -performance parameters – Basics of blade design principles Unit 7. Co. Types of power plants. 06 Hrs Fundamentals of Rocket Propulsion: Types and Classification of rockets Operating principle – Specific impulse of a rocket – Rocket nozzle classification – Rocket performance considerations Text Books 1.C. Ltd. convection. Mathur. R. Ganesan. “Rocket Propulsion Elements”. PART B Unit 5.C.Aircraft Propulsion Sub Code: Hrs/ Week: Total Hours: 10AE55 04 52 IA Marks: Exam Hours: Exam Marks: 25 03 100 PART A Unit 1. H. New York. Unit 3. “Gas Turbine. 1996 2. C.Theory of flow in isentropic nozzles – Convergent nozzles and nozzle choking – Nozzle throat conditions – Nozzle efficiency – Losses in nozzles – Over expanded and under – expanded nozzles – Ejector and variable area nozzles – Interaction of nozzle flow with adjacent surfaces – Thrust reversal. 06 Hrs Ramjet Propulsion: Operating principle – Sub critical. V. conduction. Sutton.H.R. 07 Hrs Fundamentals of Gas Turbine Engines: Illustration of working of gas turbine engine – The thrust equation – Factors affecting thrust – Effect of pressure.rocket Unit 8. and Saravanamuttoo. 5th Edn. diffusion mass transfer basic concepts and governing equations. John Wiley & Sons Inc.I. critical and supercritical operation – Combustion in ramjet engine – Ramjet performance – Sample ramjet design calculations – Introduction to scramjet – Preliminary concepts in supersonic combustion – Integral ram. 1989. G.G. G.. Rogers. “Mechanics & Thermodynamics of Propulsion” Addison – Wesley Longman INC. New York. Oates. 06 Hrs Introduction: Review of thermodynamic principles. radiation.P. 07 Hrs Subsonic and Supersonic Inlets for Jet Engines: Internal flow and Stall in subsonic inlets – Boundary layer separation – Major features of external flow near a subsonic inlet – Relation between minimum area ratio and eternal deceleration ratio – Diffuser performance – Supersonic inlets – Starting problem on supersonic inlets – Shock swallowing by area variation – External declaration – Models of inlet operation. turbofan and turbojet – Performance characteristics. AIAA Education Series. Unit 4. 07 Hrs Compressors: Principle of operation of centrifugal compressor – Work done and pressure rise – Velocity diagrams – Diffuser vane design considerations – Concept of prewhirl – Rotation stall – Elementary theory of axial flow compressor – Velocity triangles – degree of reaction – Three dimensional – Air angle distributions for free vortex and constant reaction designs – Compressor blade design – Centrifugal and Axial compressor performance characteristics.Hill. ACSCE 6 . M.. “Rolls Royce Jet Engine” – Third Edition – 1983. 1993. G... H. “Gas Turbine Theory”. velocity and temperature changes of air entering compressor – Methods of thrust augmentation – Characteristics of turboprop. “Aero thermodynamics of Aircraft Engine Components”. Longman. 06 Hrs Combustion Chambers and Nozzles: Classification of combustion chambers – Important factors affecting combustion chamber design – Combustion process – Combustion chamber performance – Effect of operating variables on performance – Flame tube cooling – Flame stabilization – Use of flame holders – . P.. Jet and Rocket Propulsion”. and Sharma.P. Tata McGraw Hill Pub. References Cohen. Principles of aircraft propulsion. Use of Aluminium alloy. 1993.G. Princeton D. Unit 4 08 Hrs Statically Determinate And Interdeterminate Structures: Analysis of plane truss – Method of joints – 3 D Truss .” Theory of Elasticity’ Mc Graw Hill Co.Castigliano's theorem . 2. frames. Edward Arnold.Aircraft Structures – I Sub Code: Hrs/ Week: Total Hours: 10AE56 04 52 IA Marks: Exam Hours: Exam Marks: 25 03 100 PART A Unit 1. 06 Hrs Materials for Aircraft Structures: Metallic and non-metallic materials. . ACSCE 7 . Dr. 1990. Department of Aeronautical Engineering. I and II. 06 Hrs Columns: Columns with various end conditions – Euler’s Column curve – Rankine’s formula . titanium. McGraw-Hill..application to beams.. strain-displacement relation. Megson. Composite beam . T. Unit 2. Plane stress and Plane strain problems in 2D elasticity and Airy’s Stress function Unit 8. Unit load method . PART B Unit 5. Von Nostrand Co. 3. Donaldson. rings.M. derivation of Equilibrium equations. Unit 6. 06 Hrs Energy Methods: Strain Energy due to axial. 06 Hrs Loads On Aircraft: Structural nomenclature – Types of loads – load factor – Aerodynamics loads – Symmetric manoeuvre loads – Velocity diagram – Function of structural components. Mechanics of Materials. “Aircraft Structures for Engineering Students”.Clapeyron's Three Moment Equation .Plane frames. Lakshmi Publication 2.Column with initial curvature . stainless steel and composite materials. B. Vol.Eccentric loading – South well plot – Beam column. Reference 1. etc. 1995. compatibility conditions and boundary conditions. Desirable properties for aircraft application Unit 3 06 Hrs Mechanical Properties of Material: Stress – Strain .BC Punmia. Arun Kumar Jain.Tensile properties – Compression properties – Shear properties – Bearing properties – Creep and Stress properties – Fracture properties –Fatigue properties. Unit 7. 08 Hrs Theory of Elasticity: Concept of stress and strain.Moment Distribution Method. Timoshenko and Goodier. trusses. 06 Hrs Failure Theory: Maximum Stress theory – Maximum Strain Theory – Maximum Shear Stress Theory – Distortion Theory – Maximum Strain energy theory – Application to aircraft Structural problems. Text Book 1.K. S..Maxwell's Reciprocal theorem. Timoshenko. “Strength of Materials”. “Analysis of Aircraft Structures – An Introduction”. Ashoak Kumar Jain. bending and Torsional loads . BP. Engine Department of Aeronautical Engineering. 4. Valve Timing/port opening diagram of an I. Calculations of IP. 10. Smoke flow visualization studies on a two dimensional airfoil at different angles of incidence at low speeds 4. 3. Thermal efficiencies. Use of planimeter.Aerodynamics Laboratory Sub Code: Hrs/ Week: Total Hours: 10AEL57 03 42 IA Marks: Exam Hours: Exam Marks: 25 03 50 LIST OF EXPERIMENTS 1. ACSCE 8 . Calibration of a subsonic wind tunnel 2. PART – B (Group Experiments) 21 Hrs 1.C. Engines. (Morse test) (d) Two stroke Petrol Engine (e) Variable Compression Ratio I. Surface pressure distributions on a two-dimensional symmetric airfoil at zero incidences at low speeds. FP. Saybolt Viscometer and Torsion viscometers. Calculation of total drag of a two-dimensional circular cylinder at low speeds using pitot-static probe wake survey. 8. Surface pressure distributions on a two-dimensional cambered airfoil at different angles of incidence and calculation of lift and pressure drag. 2. 5.C. Determination of Viscosity of lubricating oil using Redwood. 5. Calculation of total drag of a two-dimensional cambered airfoil at low speeds at incidence using pitot-static probe wake survey. SFC. Performance Tests on I. liquid and gaseous fuels 3. Energy conversion Laboratory Sub Code: Hrs/ Week: Total Hours: 10AEL58 03 42 IA Marks: Exam Hours: Exam Marks: 25 03 50 PART – A (Individual Experiments) 21 Hrs 1. engine (4 stroke/ 2stroke). Determination of Calorific value of solid. 6. heat balance sheet for (a) Four stroke Diesel Engine (b) Four stroke Petrol Engine (c) Multi-cylinder Diesel/Petrol Engine. Determination of Flash point and Fire point of lubricating oil using Abel Pensky and Pensky Martins Apparatus. Tuft flow visualization on a wing model at different angles of incidence at low speeds: identify zones of attached and separated flows.C. 9. Surface pressure distributions on a two-dimensional circular cylinder at low speeds and calculation of pressure drag. 7. Measurement of a typical boundary layer velocity profile on the tunnel wall (at low speeds) using a pitot probe and calculation of boundary layer displacement and momentum thickness. Smoke flow visualization studies on a two-dimensional circular cylinder at low speeds.