This program calculate rocket aerodynamics parameter. Calculated using Barrowman method and Apparent Mass method based on slender body theory.
BarrowmanFlow is a library for calculating aerodynamics. It is necessary to prepare driving scripts.The script describes the shape of aerodynamic elements.
"simple_rocket.py" is a simple rocket calculation example.
"fin_optimize.py" is fin optimization example.
- Interference calculation of front and rear fins
- Generalization of form plotting
- Estimate of change in Mach number - drag coefficient
- The Theoretical Prediction of the Center of Pressure
- 飛しょう体の空気力学
- NACA Technical Note 4197, SUMMARY OFV FLUTTER EXPERIENCES AS A GUIDE TO THE PRELIMINARY DESIGN OF LIFTING SURFACES ON MISSILES