Eskisehir Technical University Info Package Eskisehir Technical University Info Package
  • Info on the Institution
  • Info on Degree Programmes
  • Info for Students
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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
  • Faculty of Aeronautics and Astronautics
  • Department of Flight Training
  • Course Structure Diagram with Credits
  • Principles of Flight
  • Learning Outcomes
  • Description
  • Learning Outcomes
  • Course's Contribution to Prog.
  • Learning Outcomes & Program Qualifications

  • 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.

  • Info on the Institution
  • Name and Adress
  • Academic Calendar
  • Academic Authorities
  • General Description
  • List of Programmes Offered
  • General Admission Requirements
  • Recognition of Prior Learning
  • Registration Procedures
  • ECTS Credit Allocation
  • Academic Guidance
  • Info on Degree Programmes
  • Doctorate Degree / Proficieny in Arts
  • Master's Degree
  • Bachelor's Degree
  • Associate Degree
  • Open&Distance Education
  • Info for Students
  • Cost of living
  • Accommodation
  • Meals
  • Medical Facilities
  • Facilities for Special Needs Students ı
  • Insurance
  • Financial Support for Students
  • Student Affairs Office
  • Info for Students
  • Learning Facilities
  • International Programmes r
  • Practical Information for Mobile Students
  • Language courses
  • Internships
  • Sports and Leisure Facilities
  • Student Associations