Eskisehir Technical University Info Package Eskisehir Technical University Info Package
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About the Program Educational Objectives Key Learning Outcomes Course Structure Diagram with Credits Field Qualifications Matrix of Course& Program Qualifications Matrix of Program Outcomes&Field Qualifications
  • Vocational School Of Information Technologies
  • Electrical and Automation Department
  • Drone Technology And Operations Pr.
  • Course Structure Diagram with Credits
  • Aerodynamics
  • Learning Outcomes
  • Description
  • Learning Outcomes
  • Course's Contribution to Prog.
  • Learning Outcomes & Program Qualifications
  • ECTS Credit Load

  • Define basic principles of Aerodynamics.
  • EN: Defines physical characteristics of air and atmosphere.
  • EN: Defines basic aerodynamic forces acting on an aircraft.
  • EN: Lists the factors affecting aerodynamic forces.
  • Explains the effect of airflow on an aircraft and its components using the laws of physics and fundamental mathematical methods.
  • EN: Explains the changes in the characteristics of compressible and incompressible flows through varaible-area sections using mathematical relations.
  • EN: Calculates the airspeed, static and dynamic pressure of the flow at any point using Continuity and Bernoulli equations for one-dimensional steady flow.
  • EN: Explains the effect of viscosity on flows around flat plate and circular cylinder section.
  • EN: Explains the generation and change of aerodynamic forces on finite wings.
  • EN: Calculates aerodynamic forces and coefficients using polar equations of the wing.
  • Relates basic aerodynamic principles and practices regarding flight operations.
  • EN: Compares the aerodynamics characteristics of aircraft designed for different flight missions.
  • Defines geometric characteristics of airfoil and wings.
  • Defines aerodynamic surfaces and elements on an aircraft.
  • Defines control surfaces on an aircraft and learns their functions.
  • Relates aerodynamic characteristics and basic aircraft performance issues.
  • Calculates aerodynamic forces using pressure distributions around basic aerodynamic shapes.
  • Explain the changes of aerodynamic forces on an airfoil with respect to the geometry and configuration by drawing related graphics.

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