Propulsion system requirements of very long range, high payload aircraft relative to propulsion and laminar flow control are examined with emphasis on turbofan engines; factors influencing optimum design bypass ratio of turbofan engine and effects of laminar flow control and cargo space requirements upon optimum turbofan engine design are shown; parametric study of aircraft performance is used to compare series of industry study engines as means of showing relationship between aircraft and engine design; mission studies included offensive and defensive armed logistics, command and surveillance.
Requirements for long range -- Long endurance aircraft
SAE -- Paper
SAE Meeting ; 1964
1964
5 pages
Conference paper
English
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REQUIREMENTS FOR LONG RANGE -LONG ENDURANCE AIRCRAFT
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