| Course Unit Code | 342-0439/02 |
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| Number of ECTS Credits Allocated | 2 ECTS credits |
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| Type of Course Unit * | Choice-compulsory |
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| Level of Course Unit * | First Cycle |
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| Year of Study * | Third Year |
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| Semester when the Course Unit is delivered | Winter Semester |
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| Mode of Delivery | Face-to-face |
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| Language of Instruction | Czech |
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| Prerequisites and Co-Requisites | Course succeeds to compulsory courses of previous semester |
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| Name of Lecturer(s) | Personal ID | Name |
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| HRA56 | Josef Hranický |
| KUB925 | Ing. Martin Kubáň |
| Summary |
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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 high-speed aerodynamics of aircraft. The course builds on the Principles of Flight I
The student will gain knowledge in the field of aerodynamics, air flow around the profile at high speeds, resistance to supersonic flow, the principle and the formation of a multiple in the range that allows him to pass ATPL exams at the Civil Aviation Authority in Prague. |
| Learning Outcomes of the Course Unit |
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| 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 heavy air subsonic and supersonic speeds. Knowledge of the Principles of Flight and the need of teaching of this course by acquiring of some aviation qualifications is an ICAO requirement. |
| Course Contents |
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3 AERODYNAMICS OF SUPERSONIC SPEEDS
4.1. Oblique shock waves, special supersonic flow
4.2. Aerodynamic rating
4 STABILITY
4.3. Balance in steady horizontal flight (link)
4.4. Ways to achieve a balance (link)
4.5. Longitudinal static stability
4.6. Directional static stability
4.7. Lateral static stability
4.8. Lateral (lateral and directional) dynamic stability
5 CONTROLLABILITY
5.1. Generally, definitions and basic concepts
5.2. Longitudinal controllability
5.3. Directional controllability
5.4. Transverse controllability
5.5. Taking control yaw and roll
5.6. Ways of relieving the control forces
5.7. Mass balance rudders
5.8. Ability to trim
6 OPERATING RESTRICTIONS
6.1. List of operational limitations
6.2. Turnover envelope load
6.3. Gust load envelope
7 PROPELLER
7.1. Conversion of engine torque to thrust
7.2. Engine failure
7.3. Parameters affecting the power output of the propeller
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| Recommended or Required Reading |
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| Required Reading: |
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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
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BROŽ, V. Aerodynamika vysokých rychlostí. Praha: ČVUT v Praze, 2001. ISBN 80-01-02348-6
DANĚK, V. Mechanika letu I – Letové výkony. Brno: VUT v Brně, 1994. ISBN 80-214-0476-0
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
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| Recommended Reading: |
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KROES, M. J.; RARDON, J. R. Aircraft basic science. 7th ed. New York: Glencoe/McGraw-Hill, c1993. Glencoe aviation technology series. ISBN 0-02-801814-1.
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BROŽ, V. Aerodynamika nízkých rychlostí. Praha: ČVUT v Praze, 2001. ISBN 80-01-02347-8
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| Planned learning activities and teaching methods |
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| Lectures, Tutorials |
| Assesment methods and criteria |
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| Task Title | Task Type | Maximum Number of Points
(Act. for Subtasks) | Minimum Number of Points for Task Passing |
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| Graded exercises evaluation | Graded credit | 100 | 51 |