抄録
Take-off performance is calculated for PAR-WIG which utilizes propeller-slipstream. For this purpose, a quick automatic computation scheme is developed for performance of “engine-propeller combination system”. Example calculations are presented, which show that the hump drag is completely removed with PAR effect. It is noted that variable-geomerty of wing-end-plates is desirable and variable-camber of main-wing is essential.
© The Japan Society for Aeronautical and Space Sciences