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AIRCRAFT MODEL TO STUDY IMPACT OF JET STREAM AT AERODYNAMIC CHARACTERISTICS OF AIRCRAFT

机译:研究喷气流对飞机气动特性的影响的飞机模型

摘要

FIELD: transportation, aviation.;SUBSTANCE: aircraft model to study impact of jet stream at aerodynamic characteristics of the aircraft includes a thin-walled body fixed on a side holder with an aft nozzle and drainage holes along outer surface, drainage tubes laid in the side holder and connected to a pressure registration device, a compressed air supply system towards a model nozzle comprising a compressed air balloon, air ducts laid in the side holder and an internal cavity of the model. There are cavities arranged in the walls of the model body for placement of drainage tubes, covered by shells at the outer side and following the external contours of the model body. Drainage tubes stretch from the side holder of the model inside the arranged cavities and are joined with side channels in the body of main part of the model body. Channels are made from the side of cavities formed in the body until crossing with the external drainage holes perceiving the static pressure.;EFFECT: invention is aimed at increased validity of pressure distribution measurement results.;3 dwg
机译:领域:运输,航空;实体:用于研究射流对飞机空气动力学特性影响的飞机模型,该模型包括固定在侧支架上的薄壁主体,该侧支架上具有后喷嘴和沿外表面的排水孔,排水管位于侧支架并连接到压力记录装置,朝向模型喷嘴的压缩空气供应系统,该系统包括压缩气球,放置在侧支架中的风道和模型的内部空腔。在模型主体的壁中布置有用于放置排水管的空腔,该空腔在外侧被壳覆盖并遵循模型主体的外部轮廓。排水管从模型的侧支架延伸到布置好的空腔内,并与模型主体主要部分中的侧通道相连。通道是从体内形成的腔体的侧面制作的,直到与感知静压的外部排水孔交叉为止。效果:本发明旨在提高压力分布测量结果的有效性。3 dwg

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