Katı yakıtlı roket motorlarda 3-boyutlu yanma gerilemesi ve motor iç akış incelemesi.

In this thesis, Initial Value Problem of Level-set Method is applied to solid propellant combustion to find the grain burnback. For the performance prediction of the rocket motor, 0-D, 1-D or 3-D flow models are used depending on the type of thre grain configuration.Ph.D. - Doctoral Progra