| Defines the concept of International Standard Atmosphere (ISA) and explains the effects of physical changes in the atmosphere on flight. |
| Discusses the impact of variations in temperature, pressure, density, and altitude on aerodynamic calculations. |
| Evaluates the applicability of ISA in terms of flight performance and aerodynamic computations. |
| Describes the airflow around an object and identifies various flow types (boundary layer, laminar, and turbulent flow). |
| Defines terms such as free-stream flow, relative airflow, upwash, and downwash and explains their roles in flight dynamics. |
| Explains the phenomena of vortices and flow separation (stall), analyzing their effects on aircraft performance. |
| Defines aerodynamic terms such as angle of attack, lift coefficient, drag coefficient, aerodynamic center, and analyzes their impact on flight performance. |
| Explains profile drag, parasite drag, induced drag and discusses how each type affects flight performance. |
| Describes the effects of wing shape, roughness ratio, and smoothness ratio on flight and aircraft design. |
| Explains the relationships between lift, weight, thrust, and drag and their effects on flight dynamics. |
| Defines the concept of glide ratio, calculating it based on flight conditions. |
| Describes steady-state flight, explaining how to achieve and maintain stability during various flight phases. |
| Explains turn theory and discusses how to optimize flight during turns. |
| Analyzes the effects of load factor on flight envelope, structural limitations, and flow separation (stall). |
| Discusses methods to increase lift and improvements in aircraft design to achieve optimal aerodynamic performance. |