NASA Technical Reports Server (NTRS) : Steady pdf

NASA Technical Reports Server (NTRS) : Steady

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The effects of circumferential and radial temperature distortions and combined temperature and pressure distortion on the performance of a J85-GE-13 turbojet engine were investigated. In terms of loss of compressor pressure ratio at stall, the most severe pattern of temperature distortion was hub radial while a circumferential pattern of diametrically opposed sectors was least severe. The effect of combined temperature and pressure distortion was dependent on the location of the high temperature and low pressure regions. The most serious stall pressure ratio losses occurred when these regions coincided

• Creator/s: NASA Technical Reports Server (NTRS
• Date: 2/1/1974
• Year: 1974
• Book Topics/Themes: NASA Technical Reports Server (NTRS), ENGINE FAILURE, INLET PRESSURE, TEMPERATURE EFFECTS, TURBOJET ENGINES, COMPRESSOR EFFICIENCY, DISTORTION, PERFORMANCE TESTS, Mehalic, C. M., Lottig, R. A

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