Laboratory test were conducted to investigate the effects of vitiated inlet-air on turbojet engine performance. The test vehicle was a J60-P-6 turbojet engine which was operated at sea level hot day inlet conditions for simulated flight Mach numbers of 0.0, 0.5, and 0.85. Effects of vitiated inlet-air were evaluated at vitiation levels of 1.7, 2.3, 3.0, and 3.5 percent. (Author)
Investigation of Vitiated Inlet-Air Effects on Turbojet Engine Performance
1968
35 pages
Report
No indication
English
Analysis of turbojet-engine-inlet matching
Engineering Index Backfile | 1953
|An analysis of turbojet-engine-inlet matching
TIBKAT | 1953
|An analysis of turbojet-engine-inlet matching
NTRS | 1953
|