INVESTIGATION OF VITIATED INLET-AIR EFFECTS ON TURBOJET ENGINE PERFORMANCE
NAVAL AIR PROPULSION TEST CENTER TRENTON NJ AERONAUTICAL TURBINE DEPT
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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.
- Jet and Gas Turbine Engines