Effect of Heat and Power Extraction on Turbojet-engine Performance

Résumé du livre

For constant turbine-inlet-temperature operation the thrust decreased slightly more than double and the specific fuel consumption increased slightly less than double the percentage air bleed. There was no significant difference between variable-are and rated-area tail-pipe nozzle operation for the range of air bleeds investigated. The effect of altitude, engine-inlet temperature, and flight Mach number on engine performance with air bleed is also shown.