Spectral, directional emittance at elevated temperatures for various materials

Michael Winter, Robert Bickel, Dusan P. Sekulic, Helmut Koch, Hai Fu, Bradley Butler

Research output: Chapter in Book/Report/Conference proceedingConference contributionpeer-review

5 Scopus citations

Abstract

Material samples of stainless steel and titanium with different surface roughness values were investigated to determine their spectral directional emissivity at elevated temperatures up to 1,200 K in the visible to near infrared wavelength range (VIS/NIR) and in the infrared (IR) around 4 μm. This work supports experiments for the investigation of transition from laminar to turbulent flow and the resulting heat flux augmentation with particular respect to isolated and distributed surface roughness in the Ballistic Range Facility at NASA Ames Research Center.1The measurements of spectral directional surface emissivity were accomplished by measuring the radiation from an appropriately designed test specimen in a furnace heating facility with optical access. The blackbody radiation, needed to determine the emissivity, was generated through a cavity in the specimen itself. During the time of measurement, the sample was shielded from the furnace radiation through a retractable cold radiation shield. The potential effect of sample emission reflected from this radiation shield was investigated in a separate setup using Joule heated samples. No significant influence of this irradiation on the measured sample emission was seen so far. In the VIS/NIR, a 500 mm focal length spectrometer was used for detection. The specimen surface was imaged on the spectrometer entrance slit enabling the simultaneous measurement of a sample normal to the viewing direction, the blackbody cavity, and a tilted sample. In the IR, a FLIR camera with a band pass filer transmitting between 3.8 and 4 μm was used to image the tests specimen. In general, surface roughness was found to increase emissivity significantly in comparison to polished samples of the same material. The actual roughness values seem to have only a minor effect. The measured emissivities show only a weak variation with temperature.

Original languageEnglish
Title of host publication54th AIAA Aerospace Sciences Meeting
DOIs
StatePublished - 2016
Event54th AIAA Aerospace Sciences Meeting, 2016 - San Diego, United States
Duration: Jan 4 2016Jan 8 2016

Publication series

Name54th AIAA Aerospace Sciences Meeting
Volume0

Conference

Conference54th AIAA Aerospace Sciences Meeting, 2016
Country/TerritoryUnited States
CitySan Diego
Period1/4/161/8/16

Bibliographical note

Publisher Copyright:
© 2016, (publisher Name). All rights reserved.

Funding

This work is supported by an award from NASA Kentucky under NASA award No: NNX10AL96H. Two authors were funded in part through US NSF Grant CBET1235759 for Year 2015. The authors would like to thank Dr. Michael Wilder from NASA Ames Research Center for providing test samples and technical guidance, Frank Hui from NASA Ames Research Center for lending the pyrometer, as well as Dr. Kozo Saito and Dr. Ahmad Salaimeh of the Institute of Research for Technology Development (IR4TD) at the University of Kentucky for lending their FLIR IR camera for this research. The authors would also like to thank Floyd Taylor and Herb Mefford, University of Kentucky, for their assistance in designing and machining many of the components necessary for this project.

FundersFunder number
National Science Foundation (NSF)CBET1235759
National Aeronautics and Space AdministrationNNX10AL96H
Kentucky Space Grant Consortium
Ames Research CenterIR4TD
University of Kentucky

    ASJC Scopus subject areas

    • Aerospace Engineering

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