SUMMARY
The governing fluid flow equations for a frisbee in flight are derived from the Navier-Stokes equations. Simplifications may involve the introduction of turbulence models, as direct solutions are computationally intensive. Key references include the boundary layer problem solved by Rott and Lewellen in 1967 and the rotating infinite disc problem addressed by von Karman, with further insights available in Schlichting's and White's texts on boundary layers. These foundational works provide a starting point for theoretical derivation and experimental validation in a wind tunnel.
PREREQUISITES
- Understanding of Navier-Stokes equations
- Familiarity with turbulence models, specifically k-omega model
- Knowledge of boundary layer theory
- Experience with computational fluid dynamics (CFD) simulations
NEXT STEPS
- Research the Navier-Stokes equations in detail
- Study turbulence modeling techniques, focusing on the k-omega model
- Examine the boundary layer theory as presented in Schlichting's and White's texts
- Explore computational fluid dynamics (CFD) software for simulating fluid flow
USEFUL FOR
Aerospace engineers, fluid dynamics researchers, and students studying aerodynamics who are interested in the theoretical and practical aspects of frisbee flight dynamics.