1992 年 58 巻 556 号 p. 3653-3658
System concepts have been dealt with by applying the power augmented ram wing for large ground effect craft. Trend analysis and parametric studies on the effects of its dynamic stabilities have been conducted to evaluate some kinds of tandem wing crafts. The necessary ranges and tendencies of the aerodynamic characteristics were determined for each of the systems of enhanced lift wings. By controlling the appropriate tail unit we achieved a simulation of the flare maneuvers.