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DETERMINATION OF TIME-RESOLVED HEAT TRANSFER COEFFICIENT AND ADIABATIC EFFECTIVENESS WAVEFORMS WITH UNSTEADY FILM COOLING

机译:非稳态膜冷却法测定时间分辨的传热系数和绝热效率波形

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Traditional hot gas path film cooling characterization involves the use of wind tunnel models to measure the spatial adiabatic effectiveness (η) and heat transfer coefficient (h) distributions. Periodic unsteadiness in the flow, however, causes fluctuations in both η and h. In this paper we present a novel inverse heat transfer methodology that may be used to approximate the η(t) and h(t) waveforms. The technique is a modification of the traditional transient heat transfer technique that, with steady flow conditions only, allows the determination of η and h from a single experiment by measuring the surface temperature history as the material changes temperature after sudden immersion in the flow. However, unlike the traditional transient technique, this new algorithm contains no assumption of steadiness in the formulation of the governing differential equations for heat transfer into a semi-infinite slab. The technique was tested by devising arbitrary waveforms for η and h at a point on a film cooled surface and running a computational simulation of an actual experimental model experiencing those flow conditions. The surface temperature history was corrupted with random noise to simulate actual surface temperature measurements and then fed into an algorithm developed here that successfully and consistently approximated the η(t) and h{t) waveforms.
机译:传统的热气路径薄膜冷却特性包括使用风洞模型来测量空间绝热效率(η)和传热系数(h)分布。但是,流体的周期性不稳定会引起η和h的波动。在本文中,我们提出了一种新颖的逆传热方法,可用于近似η(t)和h(t)波形。该技术是对传统瞬态传热技术的改进,该技术仅在稳定的流动条件下,通过在材料突然浸入流中后随温度变化而测量表面温度历史记录,通过测量表面温度历史记录,通过一次实验即可确定η和h。但是,与传统的瞬态技术不同,该新算法在制定将热量传递到半无限平板中的控制微分方程时,不包含任何稳定假设。通过在薄膜冷却的表面上的某个点设计η和h的任意波形,并对遇到这些流动条件的实际实验模型进行计算仿真,对这项技术进行了测试。表面温度历史记录被随机噪声破坏,以模拟实际的表面温度测量,然后馈入此处开发的算法中,该算法成功且一致地近似了η(t)和h(t)波形。

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