Keywords = Frozen flow of combustion gases – Characteristic lines – Method of characteristics – Initial and boundary value problems – Supersonic flow – Thrust force – Specific impulse – Thrust efficiency
| Number of Articles: 1 | ||
| 1 | A COMPARISON BETWEEN FLOWS OF THREE REACTION SYSTEMS THROUGH SUPERSONIC PROPULSIVE NOZZLES | |
| Volume 13, 13th International Conference on Applied Mechanics and Mechanical Engineering., May 2008, Page 158-175 | ||
| KEMRY M. M.; EL-KADY E.A. A. | ||
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