NozzlePy
Advanced Rocket Nozzle Calculation Tool for Contour Generation, Supersonic Flow Analysis, Efficiency Evaluation and Geometry Optimization.
Now available for free.
Core Features
Contour Generation
Generation of Ideal Nozzle Contour, Truncated Ideal Contour (TIC) and Thrust Optimized Parabola (TOP) using the Method of Characteristics.
Supersonic Flow Analysis
Solving the 2D flow field to analyze Velocity, Temperature, Pressure and Density of the flow throughout the nozzle.
Boundary Layer Effects
Calculation of viscous losses and nozzle wall displacement due to boundary layer effects.
Efficiency Evaluation
Detailed assessment of nozzle efficiency by quantifying divergence, friction, and expansion losses.
Geometry Optimization
Calculation of the most efficient Nozzle Contour Parameters for TIC and TOP including Boundary Layer, Flow Separation Criterion and Geometric Restrictions.