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Computation of the normal injection of a hydrogen jet into a supersonic air flow

Computation of the normal injection of a hydrogen jet into a supersonic air flow Abstract The interaction of a planar supersonic air flow with the hydrogen jet injected perpendicularly across the slot from the duct walls is studied numerically. An algorithm is constructed for solving the Favre-averaged Navier — Stokes equations for the flow of a thermally perfect multicomponent gas based on the ENO scheme. The influence of the jet Mach number and the ratio of the jet and flow pressures on the shockwave structure of the flow and the jet penetration depth is shown. http://www.deepdyve.com/assets/images/DeepDyve-Logo-lg.png Thermophysics and Aeromechanics Springer Journals

Computation of the normal injection of a hydrogen jet into a supersonic air flow

Thermophysics and Aeromechanics , Volume 17 (4): 12 – Dec 1, 2010

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Publisher
Springer Journals
Copyright
2010 Pleiades Publishing, Ltd.
ISSN
0869-8643
eISSN
1531-8699
DOI
10.1134/S0869864310040050
Publisher site
See Article on Publisher Site

Abstract

Abstract The interaction of a planar supersonic air flow with the hydrogen jet injected perpendicularly across the slot from the duct walls is studied numerically. An algorithm is constructed for solving the Favre-averaged Navier — Stokes equations for the flow of a thermally perfect multicomponent gas based on the ENO scheme. The influence of the jet Mach number and the ratio of the jet and flow pressures on the shockwave structure of the flow and the jet penetration depth is shown.

Journal

Thermophysics and AeromechanicsSpringer Journals

Published: Dec 1, 2010

References