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A novel hovering type of fixed wing aircraft with stealth capability

机译:具有隐身能力的新型悬停式固定翼飞机

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The tactical need for fixed wing aircraft with hovering capably has long been recognized bythe military for two reasons: increased safety when landing on aircraft carriers and higher velocitiesthat the ones obtainable with rotary wing aircraft.Thus far, the only concept governing the field of vertical flight was to use thrust either from a liftfan-F35, puffer ducts –Harrier or smaller jet engines-D0 31 or Yak-141, i.e. direct lift thrust.In this paper we will look at the prospect of using a combination of the Coanda effect with theVenturi effect to generate lift by so- called “supercirculation”. This novel approach can yield manyadvantages to conventional vertical lifting by providing a more stable platform and requiring lowerpower settings – and thus lower fuel consumption.The aircraft has a fixed, negatively sweped wing that uses circulation control to achieve lift atzero air speed. The fluid used for supercirculation will come from the fan thrust reversers – which, ifcorrectly managed, can give a sufficient flow for lifting the craft and also a negative thrust componentto compensate for the positive thrust of the primary flow (not diverted).
机译:长期以来,军方已经认识到对具有可悬停能力的固定翼飞机的战术需求,原因有二:增加在航空母舰上着陆时的安全性以及旋转翼飞机所能获得的更高的速度。因此,到目前为止,这是控制垂直飞行领域的唯一概念是使用提升风扇F35的推力,或者是Harrier或更小的喷气发动机D0 31或Yak-141的推力导管,即直接提升推力。在本文中,我们将结合使用柯恩达效应和文丘里效应通过所谓的“超循环”产生升力。这种新颖的方法可提供更稳定的平台并需要较低的功率设置,从而降低了油耗,从而比传统的垂直举升具有很多优势。飞机具有固定的负向机翼,利用循环控制在零空速下实现升力。用于超级循环的流体将来自风扇反向推力器-如果正确管理,风扇反向推力器会提供足够的流量来提升飞船,并且还会产生负向推力分量,以补偿主流的正向推力(未分流)。

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