Title: 3D numerical simulation of the supersonic combustion of H<sub>2</sub>.
Authors: Dinde, Prashant; Rajasekaran, A.; Babu, V.
Abstract: The article examines three-dimensional simulation of the supersonic combustion of hydrogen dioxide. The combustor has a single stage fuel injection parallel to the main flow from the base of a wedge. The simulations have been performed using FLUENT. The RANS calculations are able to predict the mean and fluctuating quantities reasonably well in most reqions of the flow field.
Subjects: COMBUSTION; COMPUTER simulation; HYDROGEN; FUEL pumps; FLUID dynamics; HIGH-speed aeronautics; SCRAMJET engines; COMBUSTION chambers
Publication: Aeronautical Journal, 2006, Vol 110, Issue 1114, p773
ISSN: 0001-9240
Publication type: Academic Journal
DOI: 10.1017/S0001924000001640

3D numerical simulation of the supersonic combustion of H<sub>2</sub>.

Dinde, Prashant; Rajasekaran, A.; Babu, V.