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OPEN ELECTIVES OFFERED BY DEPT OF AERONATICAL ENGINEERING

               S.      COURSE      COURSE TITLE                  CATEGORY  CONTACT           L
               NO.     CODE                                                     PERIODS           T  P  C
               1        OAE1701     Introduction to Aeronautical      OE            3        3    0   0   3
                                    Engineering
               2       OAE1702      Fundamentals of Jet               OE            3        3    0   0   3
                                    Propulsion
               3        OAE1703     Introduction to space flight      OE            3        3    0   0   3

               4        OAE1704     Industrial Aerodynamics           OE            3        3    0   0   3


                                                                                            L  T  P  C
                OAE1701     INTRODUCTION TO AERONAUTICAL ENGINEERING
                                                                                            3   0  0  3

               OBJECTIVES
                     To introduce history and  classification of aircraft
                     To understand properties of atmosphere
                     To study basic aerodynamics
                     To introduce basic concepts of aircraft structure
                     To introduce piston and jet engines
                   
               UNIT I         AIRCRAFT CONFIGURATIONS                                                             8
               History  of  Flight-Wright  brothers-Different  types  of  flight  vehicles,  classification,  components  and
               functions of typical transport aircraft, Helicopter and UAV parts and functions.
               UNIT II        PROPERTIES OF ATMOSHPHERE                                                        7
               Physical  properties  and  structure  of  the  atmosphere,  ISA,  lapse  rate  –different  layer  of  atmosphere-
               different types of altitudes-temperature, pressure and altitude relationships-calculations.

               UNIT III       BASICS OF AERODYNAMICS                                                                 12
               Newton‘s law of motions applied to aeronautics - aerofoil and wing geometry, NACA series airfoils,
               generation of lift, Mach number and ranges, aerodynamic center, pressure coefs,  aspect ratio, types of
               drag, induced drag, lift and drag curves, sweepback on wing, shock waves in supersonic flight-basics of
               Pitot tube.

               UNIT IV        AIRPLANE STRUCTURES AND MATERIALS                                       9
               General types of construction, monocoque and semi-monocoque, typical wing and fuselage structure,
               metallic  and  non-metallic  materials,  use  of  aluminium  alloy,  titanium,  stainless  steel  ,  plastics,
               composite materials and applications.

               UNIT V         POWER PLANTS                                                                                        9
               Basics  about  piston,  turbojet,  turboprop  and  turbofan  -  concept  of  propeller  and  jets  for  thrust
               production , principles of operation of rocket, types of rockets and typical applications, exploration into
               space- India

                                                                                      TOTAL: 45 PERIODS
               OUTCOMES
                     Identify the types and component of aircraft
                     Understand properties of atmosphere



               Curriculum and Syllabus | Open Electives | R 2017 | REC                               Page 5
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