342-0426/01 – Principles of Flight 1 (ZL1)

Gurantor departmentInstitute of TransportCredits5
Subject guarantordoc. Ing. Vladimír Smrž, Ph.D.Subject version guarantordoc. Ing. Vladimír Smrž, Ph.D.
Study levelundergraduate or graduateRequirementCompulsory
Year1Semestersummer
Study languageCzech
Year of introduction2008/2009Year of cancellation2012/2013
Intended for the facultiesFSIntended for study typesBachelor
Instruction secured by
LoginNameTuitorTeacher giving lectures
SMR46 doc. Ing. Vladimír Smrž, Ph.D.
SOB37 Ing. Lubor Sobek, Ph.D.
Extent of instruction for forms of study
Form of studyWay of compl.Extent
Full-time Credit and Examination 3+1

Subject aims expressed by acquired skills and competences

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 and supersonic speeds. Knowledge of this subject is a civil aviation regulations requirement by acquiring of some aviation qualifications.

Teaching methods

Lectures
Seminars
Tutorials

Summary

Aerodynamics deals with the flow of fluids around the body submerged in the fluid and the forces that the flow on bodies raises. This subject deals with the aerodynamics at subsonic speeds of the airflow around the aircraft and aircraft stability.

Compulsory literature:

[1] Anderson, J. D.: Fundamentals of Aerodynamics, McGraw-Hill, New York, 1991 [2] Principles of Flight, Theoretical Knowledge Manual ATPL, Jeppesen GmbH, Frankfurt, Germany, 2001, ISBN 0-88487-290-4 [3] Thom,T.: The Aeroplane – Technical, The Air Pilot´s Manual,Volume 4, Airlife Publishing, Ltd., London, UK, 1994, ISBN 1-85310-017-X

Recommended literature:

Way of continuous check of knowledge in the course of semester

E-learning

Other requirements

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Prerequisities

Subject has no prerequisities.

Co-requisities

Subject has no co-requisities.

Subject syllabus:

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

Conditions for subject completion

Full-time form (validity from: 2006/2007 Summer semester, validity until: 2012/2013 Summer semester)
Task nameType of taskMax. number of points
(act. for subtasks)
Min. number of points
Exercises evaluation and Examination Credit and Examination 100  51
        Exercises evaluation Credit  
        Examination Examination  
Mandatory attendence parzicipation:

Show history

Occurrence in study plans

Academic yearProgrammeField of studySpec.ZaměřeníFormStudy language Tut. centreYearWSType of duty
2009/2010 (B3712) Air Transport Technology (3708R037) Aircraft Operation Technology P Czech Ostrava 1 Compulsory study plan
2009/2010 (B3712) Air Transport Technology (3708R036) Air Operation Technology P Czech Ostrava 1 Compulsory study plan
2008/2009 (B3712) Air Transport Technology (3708R037) Aircraft Operation Technology P Czech Ostrava 1 Compulsory study plan
2008/2009 (B3712) Air Transport Technology (3708R036) Air Operation Technology P Czech Ostrava 1 Compulsory study plan

Occurrence in special blocks

Block nameAcademic yearForm of studyStudy language YearWSType of blockBlock owner