To provide a vertical tailless aircraft that can improve directional stability with a simple configuration while suppressing an increase in cost.SOLUTION: A vertical tailless aircraft 10 includes: a fuselage 20 extending in an axial direction; a main wing 30 provided at a lateral face 55 of the fuselage 20; and a negative pressure generating part 40 for generating negative pressure on the lateral face 55 in a rear part of the fuselage 20 against side slip.SELECTED DRAWING: Figure 1

    【課題】コスト上昇を抑えながら、簡易な構成により方向安定性を向上することができる無垂直尾翼機を提供する。【解決手段】無垂直尾翼機10は、機軸方向に延びる胴体20と、前記胴体20の側面55に設けられた主翼30と、横滑りに対して前記胴体20の後部における側面55上に負圧を発生させる負圧発生部40と、を備えている。【選択図】図1


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    Title :

    VERTICAL TAILLESS AIRCRAFT


    Additional title:

    無垂直尾翼機


    Contributors:

    Publication date :

    2019-11-14


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    Japanese


    Classification :

    IPC:    B64C AEROPLANES , Flugzeuge



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