SUMMARY
This discussion focuses on calculating the performance of a water rocket, specifically addressing thrust, velocity, acceleration, momentum, and maximum height. Key formulas include thrust calculation using T = (π/2)PD² and height estimation with h = (Mi/Mr)²(Pi/ρg), where Mi is the mass of water, Mr is the mass of the empty rocket, Pi is the initial gauge pressure, and ρ is air density. Participants emphasize the importance of accounting for changing momentum, air pressure, and drag forces, suggesting numerical methods for more accurate results due to the complexity of the equations involved.
PREREQUISITES
- Understanding of fluid dynamics principles, particularly related to thrust and drag.
- Familiarity with basic physics equations for motion and forces.
- Knowledge of adiabatic processes and their impact on gas behavior.
- Experience with numerical methods for solving differential equations.
NEXT STEPS
- Research numerical integration techniques for dynamic systems in fluid mechanics.
- Study the effects of air density and pressure on rocket performance in varying conditions.
- Explore advanced fluid dynamics concepts such as Stokes' drag and its implications for rocket design.
- Learn about the Tsiolkovsky rocket equation and its application to water rockets.
USEFUL FOR
Students in physics, hobbyists building water rockets, and engineers interested in fluid dynamics and propulsion systems.