ACADEMY, oxford. CAE Oxford – Principles of Flight. Independently Published, 2017. ISBN 9781976743658 .
BADICK, Joseph R. a JOHNSON, Brian A. Flight theory and aerodynamics: a practical guide for operational safety. Fourth edition. Hoboken, NJ: Wiley, 2022. ISBN 978-1-119-77239-2 .
Ukončeno v akademickém roce 2020/2021
Principles of Flight 1
| Type of study | Bachelor |
|---|---|
| Language of instruction | Czech |
| Code | 342-0426/02 |
| Abbreviation | ZL1 |
| Course title | Principles of Flight 1 |
| Credits | 3 |
| Coordinating department | Institute of Transport |
| Course coordinator | Ing. David Mičulka |
Osnova předmětu
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
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