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Revising the influence of the suspension system, method and the device which raise the precision of wind tunnel measurement

机译:修正悬架系统,方法和装置的影响,提高风洞测量的精度

摘要

Revising the influence of the suspension system, the model (the aircraft model) with the suspension wire is arranged inside the wind tunnel in regard to the method of raising the precision of wind tunnel measurement, the sleeve which increases diameter of the suspension wire to effective diameter is located on the suspension wire. In order to decide field measurable quantity, effective diameter of the suspension wire and/or at diameter, 2 times or more are measured at the time of identical model building, last measurable quantity for is decided revision from the field measurable quantity of two or more the model. With 1st execution form, removing the sleeve which is inserted into the suspension wire at least at 3 stages, it makes effective diameter decrease. Last measurable quantity of drag force factor is decided from field measurable quantity by interpolation, influence of the suspension wire, revises the influence of interference of the model and the suspension wire. With another execution form, obtaining finite difference from just two field measurable quantities, it revises, without the sleeve at diameter of the suspension wire it decides one of field measurable quantities. This method is ideal in revision of the aerodynamics parameter which is due to the measurement inside the wind tunnel. In addition as for this invention it regards the device which executes this method. Selective figure Figure 1
机译:修改悬架系统的影响,关于提高风洞测量精度的方法,将带有悬架线的模型(飞机模型)布置在风洞内部,有效地增加了悬架线直径的套管直径位于吊线上。为了确定现场可测量的量,在相同的模型制造时测量悬索的有效直径和/或在直径处测量2倍或更多,最后的可测量量由两个或更多的现场可测量量决定修正该模型。在第一种实施方式中,至少在三个阶段中移除插入到悬索中的套筒,这使得有效直径减小。通过插值,吊线的影响,现场可测量的量来确定阻力系数的最后可测量量,修正模型和吊线的干扰的影响。修改了另一种执行形式,即仅从两个现场可测量的量中获得有限的差,然后修改,而无需在悬索的直径处设置套管即可确定一个现场可测量的量。这种方法是修改空气动力学参数的理想方法,这是由于风洞内部的测量所致。此外,对于本发明而言,其涉及执行该方法的装置。

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