Akademik Dersler - İçerik

Identify standard atmospheric variables and their sea level values. Compute atmospheric conditions using the universal gas laws.
Determine the pressure, the temperature and the density of the air at the specified altitude
State the relationships between indicated, calibrated, equivalent and true airspeeds and how they change with altitude and temperature.
Understand how the Pitot Tube operates
Understand how the head wind and the tail wind change the ground velocity of the aircraft
Understand lift, drag and pitching moment curves vs. angle of attack with differing wing shapes and high lift coefficient devices.
Explain characteristics of boundary layer composition caused by changes in friction and wing airfoil shape.
Examine the effects of velocity, density, area, and lift coefficient on lift and drag.
Compute stall speed and changes to stall speed due to variables such as weight load factor, altitude and lift coefficient.
Discuss how wing planform characteristics, i.e. wing area, wing span, mean aerodynamic chord, taper ratio, aspect ratio, affect lift affect drag and aircraft performance.
Examine the differences between the wing and the airfoil.
Determine maximum range, endurance speeds and rate of climb airspeeds from plots of power, thrust and drag versus airspeed and understand wind and fuel flow effects.
Understand how the altitude change effects the drag and the thrust of the aircraft
Discuss the effects of wake turbulence, ground effect and induced drag on aircraft performance and flying qualities.
Examines how the wing tip vorticies occurs and what it effects
Explain the cause and effects of compressibility and how the effects can be minimized.
Describe the required aerodynamic design criterias for the Transonic and Supersonic flights
Learn the types of Shock Waves and the ways to minimize its effects on the aircraft
Define types of stability and control with respect to axis, static, or dynamic, and the primary contributors to each type.
Understand how the center of gravity of the aircraft has an important role on the aircraft's stability