Time-Resolved Heat Transfer Measurements on the Tip Wall of a Ribbed Channel Using a Novel Heat Flux Sensor—Part I: Sensor and Benchmarks-Reference-Cited by-同舟云学术

Time-Resolved Heat Transfer Measurements on the Tip Wall of a Ribbed Channel Using a Novel Heat Flux Sensor—Part I: Sensor and Benchmarks

Published:2008-01-01 Issue:1 Volume:130 Page:
ISSN:0889-504X
Container-title:Journal of Turbomachinery
language:en
Short-container-title:

Author:

Roediger Tim¹,Knauss Helmut¹,Gaisbauer Uwe¹,Kraemer Ewald¹,Jenkins Sean²,von Wolfersdorf Jens²

Affiliation:

1. Institute of Aerodynamics and Gas Dynamics (IAG), University of Stuttgart, Pfaffenwaldring 21, Stuttgart, Germany 70569

2. Institute of Aerospace Thermodynamics (ITLR), University of Stuttgart, Pfaffenwaldring 31, Stuttgart, Germany 70569

Abstract

A novel heat flux sensor was tested that allows for time-resolved heat flux measurements in internal ribbed channels related to the study of passages in gas turbine blades. The working principle of the atomic layer thermopile (ALTP) sensor is based on a thermoelectric field created by a temperature gradient over an yttrium-barium-copper-oxide (YBCO) crystal (the transverse Seebeck effect). The sensors very fast frequency response allows for highly time-resolved heat flux measurements up to the 1MHz range. This paper explains the design and working principle of the sensor, as well as the benchmarking of the sensor for several flow conditions. For internal cooling passages, this novel sensor allows for highly accurate, time-resolved measurements of heat transfer coefficients, leading to a greater understanding of the influence of fluctuations in temperature fields.

Publisher

ASME International

Subject

Mechanical Engineering

Link

http://asmedigitalcollection.asme.org/turbomachinery/article-pdf/doi/10.1115/1.2751141/5582631/011018_1.pdf

Reference22 articles.

1. Schultz, D. L., and Jones, T. V., 1973, “Heat Transfer Measurements in Short Duration Hypersonic Facilities,” AGAR-Dograph No. 165.

2. Reduction of Data From Thin-Film Heat-Transfer Gages: A Concise Numerical Technique;Cook;AIAA J.

3. An Instrument for the Direct Measurement of Intense Thermal Radiation;Gardon;Rev. Sci. Instrum.

4. High-Frequency Response Heat-Flux Gauge;Epstein;Rev. Sci. Instrum.

5. Hayashi, M., Sakurai, A., and Aso, S., 1986, “Measurement of Heat-Transfer Coefficients in Shock Wave—Turbulent Boundary Layer Interaction Regions With a Multi-Layered Thin Film Heat Transfer Gauge,” NASA TM - 77958.

Cited by 32 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. Application of atomic layer thermopile (ALTP) sensors in organic vapor flows;2024-08-01

2. Fast-Response Thin Film Heat Flux Sensors for Harsh Environments;IEEE Sensors Journal;2024-06-15

3. High-Sensitivity Atomic Layer Thermopile Heat- Flux Sensor and Its Application in Hypersonic Low-Density Wind Tunnel Tests;IEEE Transactions on Instrumentation and Measurement;2024

4. A heat flux sensor leveraging the transverse Seebeck effect in elemental antimony;Sensors and Actuators A: Physical;2023-12

5. Angle- and Thickness-Dependent Response Characteristics of YBa₂Cu₃O_7−δ-Based Atomic-Layer Thermopile Heat Flux Sensors;IEEE Sensors Journal;2023-11-15