Hybrid Rocket Propulsion Model [Python]
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Updated
Sep 26, 2017 - Python
Hybrid Rocket Propulsion Model [Python]
Differentiable and hardware accelerated chemical kinetics simulations in python using JAX
A framework to predict ignition delay using GMM, Spath, multiple regression and error based tertiary tree algorithms to generate training models. Extreme points of the cluster are utilized to make the correct identification of cluster and test predictions.
Programas em Python utilizando Cantera para análise de combustão e cinética química.
A realistic simulation of fire propagation using thermodynamic and combustion principles, developed in Python with Pygame and NumPy
Wasserstein metric for quantitative comparison of combustion scatter data.
Physics-informed propellant combustion and nozzle performance simulator with an optional TensorFlow surrogate for specific impulse. Computes exhaust velocity, thrust, Isp, temp/pressure profiles, wall heating, and stability spectrum for multiple propellants. CLI, plots, and cached models in models
Cantera based analysis the auto-ignition of isobutanol. The associated publication: Ji, Weiqi, Peng Zhang, Tanjin He, Zhi Wang, Ling Tao, Xin He, and Chung K. Law. "Intermediate species measurement during iso-butanol auto-ignition." Combustion and Flame 162, no. 10 (2015): 3541-3553.
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