| Article ID | Journal | Published Year | Pages | File Type |
|---|---|---|---|---|
| 1715140 | Acta Astronautica | 2013 | 16 Pages |
Abstract
⺠Droplets non-uniformity in space and size effect on fuel sprays ignition was simulated numerically. ⺠Several ignition zones could be formed behind incident shock wave depending on spray properties. ⺠Increase of cloud density and decrease of droplet size create more favorable ignition conditions. ⺠Shock wave attenuation in combustible spray is studied.
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Authors
N.N. Smirnov, V.B. Betelin, A.G. Kushnirenko, V.F. Nikitin, V.R. Dushin, V.A. Nerchenko,