Adam II (Air Deflection and Modulation) propulsion system as applied to LTV propulsive wing airplane configurations which house all, or part, of their propulsion system within wing surface; briefly mentioned are original ADAM I configuration and its subsequent development to present ADAM II, together with discussion of characteristics currently used for each component such as fan turbine set, gas generator, hot gas ducting, wing mounted turbofans, and mechanical cross shafting; ADAM II concept is applicable to full spectrum of subsonic aircraft, and propulsion system uses present day state-of-art technology which makes feasibility of its development quite real.
Adam II propulsion system and internal aerodynamics
SAE -- Paper
SAE Meeting ; 1967 Propulsive wing
1967
9 pages
Conference paper
English
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ADAM II Propulsion System and Internal Aerodynamics
SAE Technical Papers | 1967
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