Course detail

Principles of Flight I

FSI-OZ1Acad. year: 2012/2013

Explaining of aerodynamic force and moment emergence on aircraft. Basic aerodynamic laws –equation of continuity, Bernoulli’s equations. Aerodynamic characteristic of profile and final wing span, 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. Swept effect, Mach number, shock waves. Aerodynamics of propeller.

Language of instruction

Czech

Number of ECTS credits

5

Mode of study

Not applicable.

Guarantor

doc. Ing. Vladimír Daněk, CSc.

Department

Institute of Aerospace Engineering (LÚ)

Learning outcomes of the course unit

The students will obtain basic knowledge and habits for application of aerodynamic relations, usable for flying activity from the point of view of piloting. They will 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.

Co-requisites

Not applicable.

Planned learning activities and teaching methods

Teaching methods depend on the type of course unit as specified in the article 7 of BUT Rules for Studies and Examinations.

Assesment methods and criteria linked to learning outcomes

Conditions for obtaining the course-unit credit: participation in the course (80% 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. Evaluation process fulfils the University requirements.

Course curriculum

Not applicable.

Work placements

Not applicable.

Aims

The goal is to familiarize students with basic problems of aerodynamics of atmospheric aircraft, principle of force 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.

Specification of controlled education, way of implementation and compensation for absences

Lectures and seminars are compulsory, and the 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 week credits are awarded at the latest.

Recommended optional programme components

Not applicable.

Prerequisites and corequisites

Not applicable.

Basic literature

Not applicable.

Recommended reading

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. (CS)
Daněk,V.: Mechanika letu I - Letové výkony. Brno: Akademické nakladatelství CERM, 2009, 293 s. ISBN 978-80-7204-659-1. (CS)
Daněk,V.: Mechanika letu II - Letové vlastnosti. Brno: Akademické nakladatelství CERM, 2011. 334 s. ISBN 978-80-7204-761-1. (CS)

Classification of course in study plans

  • Programme B2341-3 Bachelor's

    branch B-PRP , 2 year of study, winter semester, compulsory

Type of course unit

 

Lecture

26 hod., optionally

Teacher / Lecturer

doc. Ing. Vladimír Daněk, CSc.

Syllabus

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. Buffet.
13. Propellers. Propellers parameters. Basic aerodynamic characteristics of propellers.

Exercise

13 hod., compulsory

Teacher / Lecturer

doc. Ing. Vladimír Daněk, CSc.

Syllabus

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. Buffet.
13. Propellers. Propellers parameters. Basic aerodynamic characteristics of propellers.