Aircraft Performance Detailed Syllabus for B.Tech second year second sem is covered here. This gives the details about credits, number of hours and other details along with reference books for the course.<\/p>\n
The detailed syllabus for Aircraft Performance B.Tech 2016-2017 (R16) \u00a0second year second sem is as follows.<\/p>\n
B.Tech. II Year II Sem. \u00a0 \u00a0L\/T\/P\/C
\nCourse Code: AE403ES \u00a0 \u00a04\/1\/0\/4<\/p>\n
UNIT- I\u00a0Introduction To Airplane Performance:<\/strong> The role and design mission of an Aircraft, UNIT- II\u00a0Basic Aerodynamic And Propulsion Characteristics:<\/strong> Source of aerodynamic forces, UNIT- III\u00a0Airplane Performance-Steady Flight:<\/strong> Equations of motion for steady level flight, Thrust\u00a0required-graphical and analytical approach, Fundamental parameters-Thrust to Weight ratio,
\nSpecification of the Performance requirements and mission profile, Importance of\u00a0performance analysis, estimation, measurement, operational safety and economy, Scheduled\u00a0performance and operational performance of the Aircraft, The standard atmosphere, Offstandard\u00a0and design atmosphere, Measurements of air data, Air data computers.<\/p>\n
\nAerodynamic lift, drag and moment, Aerodynamic coefficients, Variation of lift, drag,\u00a0moment co-efficient, Aerodynamic centre, Lift and drag build up-Lift for the finite wing,\u00a0Wing body combinations, Drag, Drag polar, Side force, Drag reduction methods,\u00a0Aerodynamic relationships for a parabolic drag polar, Thrust and efficiency, Types of\u00a0engines, Reciprocating engines, Turbojet engines, Turbofan, Turboprop, Variation of power,\u00a0thrust, specific fuel consumption with velocity and altitude, Afterburning.<\/p>\n
\nWing loading, Lift to Drag ratio, Thrust available, Maximum velocity of the airplane, Power\u00a0required, Power available and Maximum velocity, Drag divergence mach number, Effect of\u00a0drag divergence on maximum velocity, Minimum velocity, Stall and High lift devices.\u00a0Gliding flight-Glide angle and Sinking speed, Glide range and Endurance, Climbing flight,\u00a0Rate of climb, Climb angle, Time to climb, Service and Absolute ceiling, Range-Range for a\u00a0propeller driven airplane, Range for a jet propelled airplane, Endurance- Endurance for a\u00a0propeller driven airplane, Endurance for a jet propelled airplane.<\/p>\n