Parametric study of a canard-configured transport using conceptual design optimization

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(GEN) Using an 0.8 Mach, 200 seat 3000 n.m. range transport, a program that calculates operating cost based on current information making assumptions on fleet size and production rate is used to isolate the critical design factors that determine the performance of a canard or tandem wing aircraft
(DAT) 1985

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