Local Measurement of Loss Using Heated Thin-Film Sensors

Author:

Davies M. R. D.1,O’Donnell F. K.1

Affiliation:

1. PEI Technologies: Stokes Research Institute, Department of Mechanical & Aeronautical Engineering, University of Limerick, Limerick, Ireland

Abstract

A calibration equation is derived linking the nondimensional entropy generation rate per unit area with the nondimensional aerodynamic wall shear stress and free-stream pressure gradient. It is proposed that the latter quantities, which can be measured from surface sensors, be used to measure the profile entropy generation rate. It is shown that the equation is accurate for a wide range of well-defined laminar profiles. To measure the dimensional entropy generation rate per unit area requires measurement of the thickness of the boundary layer. A general profile equation is given and used to show the range of accuracy of a further simplification to the calibration. For flows with low free-stream pressure gradients, the entropy generation rate is very simply related to the wall shear stress, if both are expressed without units. An array of heated thin film sensors is calibrated for the measurement of wall shear stress, thus demonstrating the feasibility of using them to measure profile entropy generation rate.

Publisher

ASME International

Subject

Mechanical Engineering

Cited by 6 articles. 订阅此论文施引文献 订阅此论文施引文献,注册后可以免费订阅5篇论文的施引文献,订阅后可以查看论文全部施引文献

1. Comparison of Theoretical and Semi-Empirical Solutions for Dissipation Coefficient in a Low Reynolds Number Compressor Cascade;45th AIAA Fluid Dynamics Conference;2015-06-18

2. Effect of Solidity on the Generation of Entropy in a Low Reynolds Number Compressor Cascade;2013 Aviation Technology, Integration, and Operations Conference;2013-08-08

3. Effect of Stagger Angle on the Generation of Entropy in a Low Reynolds Number Compressor Cascade;9th AIAA Aviation Technology, Integration, and Operations Conference (ATIO);2009-06-14

4. Determining the Entropy Generated in a Low Reynolds Number Compressor Cascade Based on the Wake Velocity Profile;6th AIAA Aviation Technology, Integration and Operations Conference (ATIO);2006-06-15

5. Aerodynamic Entropy Generation Rate in a Boundary Layer With High Free Stream Turbulence;Journal of Fluids Engineering;2004-07-01

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