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Propulsion System Impact on Military/Commercial STOL Transport Commonality
ISSN: 0148-7191, e-ISSN: 2688-3627
Published February 01, 1970 by SAE International in United States
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A STOL medium tactical transport featuring 1000 ft takeoff distance performance has been established utilizing the powered-lift wing to achieve STOL capability. Two powered-lift wing concepts, the augmented jet flap and the externally blown flap, are presented as optimum for a minimum thrust-to-weight ratio configuration. Interconnecting the propulsion system with engine cross ducting minimizes the unsymmetrical lift resulting from an engine failure. A commercial counterpart to the military transport is discussed.