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39717

APPLICATION OF PRESSURE SENSTIVE FOIL TECHNIQUE TO VISULAIZE SUBSONIC JET FLOW OVER A PLATE

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Last updated: 04 Jan 2025

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Abstract

ABSTRACT
The present study proposes new technique to implement pressure sensitive coating on
porous anodized aluminum. The new technique is called pressure sensitive foil (PSFoil).
It is based on the conventional anodized aluminum pressure sensitive paint (AAPSP)
technique. In this technique, a very thin aluminum foil is coated with pressure
sensitive paint using anodization method. The resulting pressure sensitive foil (PS-Foil)
can be stick over any flat surface using a very thin silicon layer. The PS-Foil technique
shows very fast time response as conventional porous anodized aluminum and high
spatial resolution compared with conventional PSP binder based techniques. It can also
be applied to any existing model surface without the need to fabricate the model from
aluminum. The total thickness of the aluminum foil and silicon layer is as small as 250
micro-meters. The paint employed in the present research is Bathophen Ruthenium
Chloride (Ru(ph2-phen) or Ru(dpp) ). Commercially available inexpensive, high quality,
14-bit, CCD camera is used to capture the PSP images. Intensity based method and
"in-situ" calibration procedure are used to obtain the calibrated PSP images. The
proposed technique was applied to measure the pressure distribution over a flat plate
due to subsonic jet impingement at different impingement angles. The resulting PSP
images showed high spatial resolution of the pressure distribution and pressure
difference as low as 0.5 kPa can be measured.

DOI

10.21608/amme.2008.39717

Keywords

Pressure Sensitive Paints (PSP), Pressure Sensitive Foil Technique, Subsonic Jet, Jet- Plate Impingement, Bathophen Ruthenium Chloride, and in-situ Calibration Technique

Authors

First Name

IBRAHIM

Last Name

K.

MiddleName

M.

Affiliation

Lecturer, Aerospace Engineering Department, Faculty of Engineering, University of Cairo, Giza, 12613 Egypt.+, Currently Assistant Professor, Aerospace Engineering Department, Graduate School of Engineering, Nagoya University, Nagoya 464-8603, Japan.

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First Name

MORI

Last Name

K.

MiddleName

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Affiliation

Lecturer, Aerospace Engineering Department, Graduate School of Engineering, Nagoya University, Furo-cho, Chikusa-ku, Nagoya 464-8603, Japan.

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First Name

NAKAMURA

Last Name

Y.

MiddleName

-

Affiliation

Professor, Aerospace Engineering Department, Graduate School of Engineering, Nagoya University, Furo-cho, Chikusa-ku, Nagoya 464-8603, Japan.

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Volume

13

Article Issue

13th International Conference on Applied Mechanics and Mechanical Engineering.

Related Issue

6264

Issue Date

2008-05-01

Receive Date

2019-07-08

Publish Date

2008-05-01

Page Start

404

Page End

415

Print ISSN

2636-4352

Online ISSN

2636-4360

Link

https://amme.journals.ekb.eg/article_39717.html

Detail API

https://amme.journals.ekb.eg/service?article_code=39717

Order

109

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Original Article

Type Code

831

Publication Type

Journal

Publication Title

The International Conference on Applied Mechanics and Mechanical Engineering

Publication Link

https://amme.journals.ekb.eg/

MainTitle

APPLICATION OF PRESSURE SENSTIVE FOIL TECHNIQUE TO VISULAIZE SUBSONIC JET FLOW OVER A PLATE

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Article

Created At

22 Jan 2023