SUMMARY
This discussion focuses on calculating vertical forces experienced by a light aircraft during landing, specifically using the sink rate and landing weight. Participants emphasize the importance of understanding the change in momentum, represented by the formula F = Δp/Δt, where p = mv. The conversation highlights the challenges posed by ground effect and external factors like turbulence, which complicate accurate force calculations. Additionally, the use of Finite Element Analysis (FEA) software, specifically ANSYS Workbench, is suggested for modeling these forces more accurately.
PREREQUISITES
- Understanding of basic physics principles, particularly momentum and force calculations.
- Familiarity with Finite Element Analysis (FEA) concepts and tools, specifically ANSYS Workbench.
- Knowledge of aerodynamics, including ground effect and its impact on landing dynamics.
- Experience with aircraft design principles, particularly those related to landing gear dynamics.
NEXT STEPS
- Research the application of FEA in modeling aircraft landing dynamics using ANSYS Workbench.
- Study the effects of ground effect on landing performance and how to account for it in calculations.
- Explore the dynamic behavior of landing gear systems and factors affecting their performance during touchdown.
- Review "Airplane Design Part IV" by Roskam for methodologies on calculating kinetic energy absorption during landing.
USEFUL FOR
Aerospace engineers, aircraft designers, and students studying aerodynamics or structural analysis who are interested in understanding and modeling landing forces on aircraft.