首页> 外文会议>European rotorcraft forum >MEASUREMENT OF PEAK TEMPERATURE RISE ABOVE HELICOPTER PLATFORMS DUE TO HOT GAS PLUMES: INTERPRETATION AND EVALUATION OF REGULATIONS ON TURBULENCE AND HOT GAS PLUMES
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MEASUREMENT OF PEAK TEMPERATURE RISE ABOVE HELICOPTER PLATFORMS DUE TO HOT GAS PLUMES: INTERPRETATION AND EVALUATION OF REGULATIONS ON TURBULENCE AND HOT GAS PLUMES

机译:高温气雾导致直升机平台上方峰值温度的测量:湍流和高温气雾规则的解释和评估

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摘要

Turbulence and temperature rise criteria for helicopter platforms are defined in CAP 437. To the authors opinion there is no discussion on the relevance of these criteria. Guidance on the assessment techniques should be improved however as the current guidance seems to advise some techniques that cannot evaluate the physical properties defined in the criteria. Also guidance on the practical use of the results of the temperature rise assessment would be very useful. At the current state of the art the assessment of the turbulence and temperature rise criteria can only be made in a properly scaled buoyant plume wind tunnel experiment. Suggestions for improvement of the guidance on interpretation and evaluation are given.
机译:CAP 437定义了直升机平台的湍流和温升标准。作者认为,这些标准的相关性没有讨论。但是,由于目前的指南似乎建议一些无法评估标准中定义的物理性质的技术,因此应改进有关评估技术的指南。关于温升评估结果的实际使用的指导也将是非常有用的。在当前的现有技术中,只能在适当规模的浮力羽状风洞实验中对湍流和温升标准进行评估。提出了改进解释和评价指南的建议。

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