Abstract :
[en] With the difficulty and cost of full-scale flight experiments, the design of scramjet engines
relies heavily on computational simulations. Radiation may play an important role in wall
heating and flow cooling of scramjets. However, very few studies have focused on such. The present analysis is based on three-dimensional turbulent reacting flow simulations of
the HyShot II hydrogen fueled scramjet engine running at flight conditions of Mach 7.4. A
one-dimensional Discrete Ordinates Method analysis with a narrow band averaged spectral
model is employed to determine wall heating and flow cooling from thermal radiation. The
one-dimensional Discrete Ordinates Method is verifi ed against a three-dimensional ray
tracing method. The radiative species considered are H2O and OH. The radiative heat flux
is on the order of 10 kW/m2, which is 0.1-0.2% of the total convective wall heat flux. Flow
cooling due to radiation is found to be on the order of 2 K. Sensitivity analysis shows that
radiation is highly dependent on chamber size, temperature, pressure and radiative species
mole fraction. Variations in these factors can explain the differences between previous
analyses in the literature that studied hypothetical engines and the current work that
models an existing scramjet.
Crow, Andrew J.; University of Michigan, Ann Arbor, MI, 48105
Boyd, Iain D.; University of Michigan, Ann Arbor, MI, 48105
Publisher :
Curran Associates, Inc., Red Hook, United States - New York
Scopus citations®
without self-citations
8