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HYBRID COMPUTER MODELS AS AN AID IN DESIGN OF GAS TURBINE CONTROL SYSTEMS FOR HELICOPTERS.LANGTON R; EVANS RM; MACISAAC BD et al.1977; QUART. BULL. DIV. MECH. ENGNG NATION. AERONAUT. ESTABL.; CANADA; DA. 1977; NO 3; PP. 1-12; BIBL. 8 REF.Article