Akademik Dersler - İçerik

D steady flow.
Defines physical charfacteristics of air and atmosphere
Defines basic aerodynamic forces acting on an aircraft
Lists the factors affecting aerodynamic forces
Defines geometric characteristics of airfoil and wing
Defines aerodynamic devices on an aircraft
explains the effect of airflow on an aircraft and its components using the laws of physics and fundamental mathematical methods
Explains the changes in the characteristics of compressible and incompressible
Calculates the airspeed, static and dynamic pressure of the flow at any point using Continuity and Bernoulli equations for
Explains the generation of aerdynamic forces on airfoils and wings.
Explains the changes of aerodynamic forces on an airfoil with respect to the geometry and configuration by drawing related graphics
Explains the effect of viscosity on flows arround various shapes.
Explains the generation and change of aerodynamic forces on finite wings
Calculates aerodyamic forces and coefficients using polar equation of the wing.
relates basic aerodynamic principles and practices regarding flight operations
Compares the aerodynamics characteristics of aircraft designed for different flight missions
Relates aerodynamic characteristics and basic aircraft perfornance issues.
Defines the stability and control characteristics of aircraftabout three axes
Defines the movements of aircraft about stability axes.
Defines stabilty and control surfaces
Explains the difference between static and dynamic stability
Describes how control surfaces function
Describes the working principle and thrust generation of propellers
Describes straight level flight, climb, descend, gliding and turning maneuvers using basic mathematical relations.