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
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, Pages 158-175

10.21608/amme.2008.39262

KEMRY M. M.; EL-KADY E.A. A.

The International Conference on Applied Mechanics and Mechanical Engineering

Journal Archive