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Internet Research on the subject |
8.1 Atmospheric Physics
International Standard Atmosphere (ISA) and its application in aerodynamics. |
Visual supported Direct Lecture |
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Internet Research on the subject |
8.1 Atmospheric Physics
International Standard Atmosphere (ISA) and its application in aerodynamics.
8.2 Aerodynamics
Airflow around an object:
Boundary layer, laminar and turbulent flow, free-stream flow, relative airflow, upwash and downwash, vortices, and flow separation (stall).
Terms:
Angle of attack, aerodynamic chord, average aerodynamic chord, profile (parasite) drag, induced drag, pressure center, roughness ratio, smoothness ratio, wing shape, and aspect ratio.
Forces in flight:
Thrust, weight, aerodynamic resultant.
Lift and drag formation:
Angle of attack, lift coefficient, drag coefficient, polar slope, stall (perdovites).
Profile contaminants:
Ice, snow, and frost accumulation on the airfoil. |
Visual supported Direct Lecture |
| 3 |
Internet Research on the subject |
8.2 Aerodynamics
Airflow around an object:
Boundary layer, laminar and turbulent flow, free-stream flow, relative airflow, upwash and downwash, vortices, and flow separation (stall).
Terms:
Angle of attack, aerodynamic chord, average aerodynamic chord, profile (parasite) drag, induced drag, pressure center, roughness ratio, smoothness ratio, wing shape, and aspect ratio.
Forces in flight:
Thrust, weight, aerodynamic resultant.
Lift and drag formation:
Angle of attack, lift coefficient, drag coefficient, polar slope, stall (perdovites).
Profile contaminants:
Ice, snow, and frost accumulation on the airfoil. |
Visual supported Direct Lecture |
| 4 |
Internet Research on the subject |
8.2 Aerodynamics
Airflow around an object:
Boundary layer, laminar and turbulent flow, free-stream flow, relative airflow, upwash and downwash, vortices, and flow separation (stall).
Terms:
Angle of attack, aerodynamic chord, average aerodynamic chord, profile (parasite) drag, induced drag, pressure center, roughness ratio, smoothness ratio, wing shape, and aspect ratio.
Forces in flight:
Thrust, weight, aerodynamic resultant.
Lift and drag formation:
Angle of attack, lift coefficient, drag coefficient, polar slope, stall (perdovites).
Profile contaminants:
Ice, snow, and frost accumulation on the airfoil. |
Visual supported Direct Lecture |
| 5 |
Internet Research on the subject |
8.2 Aerodynamics
Airflow around an object:
Boundary layer, laminar and turbulent flow, free-stream flow, relative airflow, upwash and downwash, vortices, and flow separation (stall).
Terms:
Angle of attack, aerodynamic chord, average aerodynamic chord, profile (parasite) drag, induced drag, pressure center, roughness ratio, smoothness ratio, wing shape, and aspect ratio.
Forces in flight:
Thrust, weight, aerodynamic resultant.
Lift and drag formation:
Angle of attack, lift coefficient, drag coefficient, polar slope, stall (perdovites).
Profile contaminants:
Ice, snow, and frost accumulation on the airfoil. |
Visual supported Direct Lecture |
| 6 |
Internet Research on the subject |
8.2 Aerodynamics
Airflow around an object:
Boundary layer, laminar and turbulent flow, free-stream flow, relative airflow, upwash and downwash, vortices, and flow separation (stall).
Terms:
Angle of attack, aerodynamic chord, average aerodynamic chord, profile (parasite) drag, induced drag, pressure center, roughness ratio, smoothness ratio, wing shape, and aspect ratio.
Forces in flight:
Thrust, weight, aerodynamic resultant.
Lift and drag formation:
Angle of attack, lift coefficient, drag coefficient, polar slope, stall (perdovites).
Profile contaminants:
Ice, snow, and frost accumulation on the airfoil. |
Visual supported Direct Lecture |
| 7 |
Internet Research on the subject |
8.3 Flight Theory
The relationship between lift, weight, thrust, and drag.
Glide ratio.
Steady-state flight and performance.
Turn theory.
Load factor effect:
Stall, flight envelope, and structural limitations.
Increase of lift. |
Visual supported Direct Lecture |
| 8 |
Internet Research on the subject |
8.3 Flight Theory
The relationship between lift, weight, thrust, and drag.
Glide ratio.
Steady-state flight and performance.
Turn theory.
Load factor effect:
Stall, flight envelope, and structural limitations.
Increase of lift. |
Visual supported Direct Lecture |
| 9 |
Internet Research on the subject |
8.3 Flight Theory
The relationship between lift, weight, thrust, and drag.
Glide ratio.
Steady-state flight and performance.
Turn theory.
Load factor effect:
Stall, flight envelope, and structural limitations.
Increase of lift. |
Visual supported Direct Lecture |
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MID-TERM EXAM |
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| 11 |
Internet Research on the subject |
8.3 Flight Theory
The relationship between lift, weight, thrust, and drag.
Glide ratio.
Steady-state flight and performance.
Turn theory.
Load factor effect:
Stall, flight envelope, and structural limitations.
Increase of lift. |
Visual supported Direct Lecture |
| 12 |
Internet Research on the subject |
8.3 Flight Theory
The relationship between lift, weight, thrust, and drag.
Glide ratio.
Steady-state flight and performance.
Turn theory.
Load factor effect:
Stall, flight envelope, and structural limitations.
Increase of lift. |
Visual supported Direct Lecture |
| 13 |
Internet Research on the subject |
8.3 Flight Theory
The relationship between lift, weight, thrust, and drag.
Glide ratio.
Steady-state flight and performance.
Turn theory.
Load factor effect:
Stall, flight envelope, and structural limitations.
Increase of lift. |
Visual supported Direct Lecture |
| 14 |
Internet Research on the subject |
8.3 Flight Theory
The relationship between lift, weight, thrust, and drag.
Glide ratio.
Steady-state flight and performance.
Turn theory.
Load factor effect:
Stall, flight envelope, and structural limitations.
Increase of lift.
8.4 Flight Stability and Dynamics
Longitudinal, lateral, and directional stability (both active and passive). |
Visual supported Direct Lecture |
| 15 |
Internet Research on the subject |
8.4 Flight Stability and Dynamics
Longitudinal, lateral, and directional stability (both active and passive). |
Visual supported Direct Lecture |
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FINAL EXAM |
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FINAL EXAM |
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