Principles of Flight I (FSI-OZ1)

Academic year 2021/2022
Supervisor: Ing. Pavel Zikmund, Ph.D.  
Supervising institute: LÚ all courses guaranted by this institute
Teaching language: Czech
Aims of the course unit:
The goal is to familiarize students with the basic aerodynamics of atmospheric aircraft, the principle of forces and moments emergence on aircraft. Students will learn to apply practically their knowledge of aerodynamics in pilot practice for the purpose of higher flight safety.
Learning outcomes and competences:
The students gain basic knowledge and habits for the aerodynamic application usable for flying from the piloting point of view. They acquire knowledge of flying theory necessary for effective and safe aircraft traffic.
Prerequisites:
The basics of mathematics - differential and integral calculus, common differential equations. The basics of common mechanics – force effect on a body, kinematics and dynamics. The basics of fluid mechanics.
Course contents:
Explaining of aerodynamic force and moment emergence on aircraft. Basic aerodynamic laws –equation of continuity, Bernoulli’s equations. Aerodynamic characteristic of profile and finite aspect ratio wing, drag due to lift. Aircraft aerodynamic characteristic – parasitic drag, interferential drag. High lift and drag devices. Compressibility effect on aircraft aerodynamic characteristic – subsonic, transonic, and supersonic speeds. The swept effect, Mach number, shock waves.
Teaching methods and criteria:
The course is taught through lectures explaining the basic principles and theory of the discipline. Exercises are focused on practical topics presented in lectures.
Assesment methods and criteria linked to learning outcomes:
Conditions for obtaining the course-unit credit: participation in the course (95% at the minimum), presentation of calculation tasks records. The credit is necessary to be admitted to examinations. The exam has written form (the essential one) and oral parts. The evaluation process fulfills the University requirements.
Controlled participation in lessons:
Lectures and seminars are compulsory, and attendance is checked and recorded. The absence (15%-20%) can be compensated by personal consultation with the lecturer and elaboration of individually assigned topics and exercises. All tasks must be finished and handed in the credit week at the latest.
Type of course unit:
    Lecture  13 × 2 hrs. compulsory                  
    Exercise  13 × 1 hrs. compulsory                  
Course curriculum:
    Lecture 1. Basics, definitions and laws. Equation of continuity. Bernoulli´s equation.
2. Airfoil aerodynamic forces and moments. Airfoil coefficients.
3. Viscosity effects. Boundary layer. Reynold´s number. Flow separation.
4. Aerodynamic characteristic of wings. Induced drag.
5. Airplane aerodynamic characteristics. Interference drag. Total drag of airplane.
6. Means of increasing lift. Influence of ground effect.
7. Stall. Stall speeds.
8. Means of increasing drag. Spoilers. Aerodynamic brakes.
9. Influence of ice and contamination on the aerodynamic characteristics.
10. Compressibility efects. Speed of sound. Mach number.
11. Subsonic, transonic and supersonic speed aerodynamics. Critical Mach number.
12. Shock waves. Normal and oblique shock waves. Expansion waves.
13. Buffet onset. Buffet free range. "Coffin corner".
    Exercise 1. Basics, definitions and laws. Equation of continuity. Bernoulli´s equation.
2. Airfoil aerodynamic forces and moments. Airfoil coefficients.
3. Viscosity effects. Boundary layer. Reynold´s number. Flow separation.
4. Aerodynamic characteristic of wings. Induced drag.
5. Airplane aerodynamic characteristics. Interference drag. Total drag of airplane.
6. Means of increasing lift. Influence of ground effect.
7. Stall. Stall speeds.
8. Means of increasing drag. Spoilers. Aerodynamic brakes.
9. Influence of ice and contamination on the aerodynamic characteristics.
10. Compressibility effect. Speed of sound. Mach number.
11. Subsonic, transonic and supersonic speed aerodynamics. Critical Mach number.
12. Shock waves. Normal and oblique shock waves. Expansion waves. Buffet.
13. Propellers. Propellers parameters. Basic aerodynamic characteristics of propellers.
Literature - recommended:
1. Daněk,V.- Filakovský,K.: Základy letu. Učební texty pro teoretickou přípravu dopravních pilotů dle předpisu JAR-FCL-1. Brno: Akademické nakladatelství CERM, 2006. 314 s. ISBN 80-7104-449-4.
2. Daněk,V.: Mechanika letu I - Letové výkony. Brno: Akademické nakladatelství CERM, 2009, 293 s. ISBN 978-80-7204-659-1.
3. Daněk,V.: Mechanika letu II - Letové vlastnosti. Brno: Akademické nakladatelství CERM, 2011. 334 s. ISBN 978-80-7204-761-1.
The study programmes with the given course:
Programme Study form Branch Spec. Final classification   Course-unit credits     Obligation     Level     Year     Semester  
B-PRP-P full-time study --- no specialisation -- GCr 4 Compulsory 1 2 W