Background and development program; list of current applications for engine; selection of airflow capacity at approximately 50 lb/sec; factors considered in choice of 9-stage compressor to maintain max relative Mach number at 1.0 and average stage pressure ratio at 1. 24; use of IBM calculation in compressor design procedure; comparison of JT12 with JT4 relating to various design features.
JT12 Pratt and Whitney aircraft's 3000 Lb. Thrust turbojet engine
SAE -- Paper
SAE Meeting ; 1959 Pratt and Whitney
1959
14 pages
Conference paper
English
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THE JT12 PRATT & WHITNEY AIRCRAFT'S 3000 LB. THRUST TURBOJET ENGINE
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