4   Artículos

 
en línea
Jiahao Liu, Yinghong Wang, Xinyang Li and Junhao Cong    
A new method for determining the burning rate of a solid propellant, called the Impulse Method, is proposed in this paper. It is based on the proportional relationship between the impulse generated and the mass of the burned propellant. The pressure?time... ver más
Revista: Aerospace    Formato: Electrónico

 
en línea
Giuseppe Daniele Di Martino, Carmine Carmicino, Stefano Mungiguerra and Raffaele Savino    
The computational fluid dynamics of hybrid rocket internal ballistics is becoming a key tool for reducing the engine operation uncertainties and development cost as well as for improving experimental data analysis. Nevertheless, its application still pre... ver más
Revista: Aerospace    Formato: Electrónico

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