| Article ID | Journal | Published Year | Pages | File Type |
|---|---|---|---|---|
| 8056749 | Acta Astronautica | 2015 | 7 Pages |
Abstract
Analytical and physical models of gasification for model liquid fuels are developed. Numerical and experimental modeling of heat and mass transfer processes were completed with convective and irradiative heat exchange during hot gas flow (heat carrier) into the closed volume with the residual liquid. The heat carrier gas parameters were the following: temperature of the heat carrier, 373±2K; temperature of the surroundings, 291±2K; and flow rate of the heat carrier, 300l/min.
Keywords
Related Topics
Physical Sciences and Engineering
Engineering
Aerospace Engineering
Authors
V.I. Tryshlyakov, S.A. Lavruk,