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Principles of Flight 1

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Course Unit Code342-0426/03
Number of ECTS Credits Allocated3 ECTS credits
Type of Course Unit *Choice-compulsory
Level of Course Unit *First Cycle
Year of Study *Second Year
Semester when the Course Unit is deliveredWinter Semester
Mode of DeliveryFace-to-face
Language of InstructionCzech
Prerequisites and Co-Requisites Course succeeds to compulsory courses of previous semester
Name of Lecturer(s)Personal IDName
HRA56Josef Hranický
SMR46doc. Ing. Vladimír Smrž, Ph.D.
SOB37Ing. Lubor Sobek, Ph.D.
KUB925Ing. Martin Kubáň
Summary
The course is based on module 080, the basics of flight in Annex I to Commission Regulation (EU) 1178/2011, which lays down the technical requirements for crews in civil aviation under Regulation (EC) No 216/2008 of the European Parliament and of the Council. The content is focused on the basic knowledge of low-speed aerodynamics of aircraft.
The student will gain knowledge in the field of aerodynamics, air flow around the profile, the formation of resistance, the principle of propeller operation and the basics of high-speed flow to the extent that allows him to pass ATPL exams at the Civil Aviation Authority in Prague.
Learning Outcomes of the Course Unit
The subject´s goal is to achieve the necessary competencies to focus on the issues of fundamental principles of aircraft flying in the areas of subsonic speeds. Knowledge of this subject is a civil aviation regulations requirement by acquiring of some aviation qualifications.
Course Contents
1 AERODYNAMICS OF SUBSONIC SPEEDS
1.1. Physical principles, laws and definitions
1.2. Two-dimensional flow past airfoils
1.3. Aerodynamic coefficient
1.4. Three-dimensional flow around an airplane
1.5. The total resistance of the airplane
1.6. Ground Effect
1.7. The relationship between lift coefficient and speed constant buoyancy
1.8. Flow separation on the wing
1.9. Increasing the maximum lift coefficient
1.10. Means to reduce the proportion of CL-CD, and to increase resistance
1.11. Boundary layer (link)
1.12. Special cases - special circumstances

2 AERODYNAMICS OF TRANSSONIC SPEEDS
2.1. The definition of Mach number
2.2. Shock waves
2.3. Ways to avoid the effects of exceeding the critical Mach number
Recommended or Required Reading
Required Reading:
ANDERSON, J. D. Fundamentals of Aerodynamics, McGraw-Hill, New York, 1991.
Principles of Flight, Theoretical Knowledge Manual ATPL. Frankfurt: Jeppesen GmbH, 2001. ISBN 0-88487-290-4.
THOM, T. The Aeroplane – Technical, The Air Pilot´s Manual, Volume 4. London: Airlife Publishing, Ltd., 1994. ISBN 1-85310-017-X.
ANDERSON, J. D. Fundamentals of Aerodynamics, McGraw-Hill, New York, 1991.
BROŽ, V. Aerodynamika nízkých rychlostí. Praha: ČVUT v Praze, 2001. ISBN 80-01-02347-8.
Principles of Flight, Theoretical Knowledge Manual ATPL. Frankfurt: Jeppesen GmbH, 2001. ISBN 0-88487-290-4.
THOM, T. The Aeroplane – Technical, The Air Pilot´s Manual, Volume 4. London: Airlife Publishing, Ltd., 1994. ISBN 1-85310-017-X.
Recommended Reading:
ANDERSON, J. D. Fundamentals of Aerodynamics, McGraw-Hill, New York, 1991.
Principles of Flight, Theoretical Knowledge Manual ATPL. Frankfurt: Jeppesen GmbH, 2001. ISBN 0-88487-290-4.
THOM, T. The Aeroplane – Technical, The Air Pilot´s Manual, Volume 4. London: Airlife Publishing, Ltd., 1994. ISBN 1-85310-017-X.
DANĚK, V. Mechanika letu I – Letové výkony. Brno: VUT v Brně, 1994. ISBN 80-214-0476-0.
BROŽ, V. Aerodynamika vysokých rychlostí. Praha: ČVUT v Praze, 2001. ISBN 80-01-02348-6.
Planned learning activities and teaching methods
Lectures, Seminars, Tutorials
Assesment methods and criteria
Task TitleTask TypeMaximum Number of Points
(Act. for Subtasks)
Minimum Number of Points for Task Passing
Credit and ExaminationCredit and Examination100 (100)51
        CreditCredit30 16
        ExaminationExamination70 21