The paper “A Quasi-One-Dimensional Model of Hydrogen-Fueled Scramjet Combustors” by Drs. Cristian Birzer and Con J. Doolan has been accepted for publication in the Journal of Propulsion and Power.
See all Dr Doolan’s papers here.
Abstract:
A computationally efficient, quasi-one-dimensional supersonic combustion ram- jet (scramjet) propulsion model has been produced for use in hypersonic system design studies. The model solves a series of ordinary differential equations us- ing a 4th order Runga-Kutta method, to describe the gas dynamics within the scramjet duct. Additional models for skin friction and wall heat transfer are also included. The equations are derived assuming an open thermodynamic system with equilibrium or simplified chemistry combustion models. The combustion is also assumed to be mixing rather than kinetically limited. This assumption allows simplification of the modelling and is justified when the model is compared against experimental results. Three test cases are used to validate the performance of the scramjet propulsion model: (1) modelling a reflected shock tunnel hydrogen fu- elled scramjet experiment, (2) a continuous flow hydrogen fuelled scramjet ground test and (3) a segment of the HyShot II flight test. The results show that the model simulates scramjet propulsion with a reasonable degree of accuracy.





