Development of a new pressure sensitive luminescent coating

M. Hamner, Arnold Anthony Fontaine, P. Atsavapranee

Research output: Chapter in Book/Report/Conference proceedingConference contribution

3 Citations (Scopus)

Abstract

New types of pressure sensitive luminescent coatings have been developed. These coatings sense changes in pressure directly, rather than oxygen as did previous pressure sensitive paints. Therefore, these coatings can operate in virtually any test environment, e.g. water, nitrogen or air. Two distinct wavelengths of light are emitted from these coatings allowing "ratiometric" data reduction that eliminates the need for "wind-off" or reference data saving time and money. Initial calibration results and results from the first test of these coatings at Pennsylvania State University/Applied Research Laboratory's Twelve-Inch Water Tunnel are presented in this paper.

Original languageEnglish (US)
Title of host publication41st Aerospace Sciences Meeting and Exhibit
StatePublished - 2003
Event41st Aerospace Sciences Meeting and Exhibit 2003 - Reno, NV, United States
Duration: Jan 6 2003Jan 9 2003

Other

Other41st Aerospace Sciences Meeting and Exhibit 2003
CountryUnited States
CityReno, NV
Period1/6/031/9/03

Fingerprint

coating
coatings
Coatings
hydraulic test tunnels
pressure sensitive paints
data reduction
Research laboratories
Paint
Wind tunnels
Water
Data reduction
tunnel
Calibration
Nitrogen
calibration
wavelength
nitrogen
Wavelength
water
oxygen

All Science Journal Classification (ASJC) codes

  • Space and Planetary Science
  • Aerospace Engineering

Cite this

Hamner, M., Fontaine, A. A., & Atsavapranee, P. (2003). Development of a new pressure sensitive luminescent coating. In 41st Aerospace Sciences Meeting and Exhibit
Hamner, M. ; Fontaine, Arnold Anthony ; Atsavapranee, P. / Development of a new pressure sensitive luminescent coating. 41st Aerospace Sciences Meeting and Exhibit. 2003.
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Hamner, M, Fontaine, AA & Atsavapranee, P 2003, Development of a new pressure sensitive luminescent coating. in 41st Aerospace Sciences Meeting and Exhibit. 41st Aerospace Sciences Meeting and Exhibit 2003, Reno, NV, United States, 1/6/03.

Development of a new pressure sensitive luminescent coating. / Hamner, M.; Fontaine, Arnold Anthony; Atsavapranee, P.

41st Aerospace Sciences Meeting and Exhibit. 2003.

Research output: Chapter in Book/Report/Conference proceedingConference contribution

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AU - Fontaine, Arnold Anthony

AU - Atsavapranee, P.

PY - 2003

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N2 - New types of pressure sensitive luminescent coatings have been developed. These coatings sense changes in pressure directly, rather than oxygen as did previous pressure sensitive paints. Therefore, these coatings can operate in virtually any test environment, e.g. water, nitrogen or air. Two distinct wavelengths of light are emitted from these coatings allowing "ratiometric" data reduction that eliminates the need for "wind-off" or reference data saving time and money. Initial calibration results and results from the first test of these coatings at Pennsylvania State University/Applied Research Laboratory's Twelve-Inch Water Tunnel are presented in this paper.

AB - New types of pressure sensitive luminescent coatings have been developed. These coatings sense changes in pressure directly, rather than oxygen as did previous pressure sensitive paints. Therefore, these coatings can operate in virtually any test environment, e.g. water, nitrogen or air. Two distinct wavelengths of light are emitted from these coatings allowing "ratiometric" data reduction that eliminates the need for "wind-off" or reference data saving time and money. Initial calibration results and results from the first test of these coatings at Pennsylvania State University/Applied Research Laboratory's Twelve-Inch Water Tunnel are presented in this paper.

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Hamner M, Fontaine AA, Atsavapranee P. Development of a new pressure sensitive luminescent coating. In 41st Aerospace Sciences Meeting and Exhibit. 2003