Pressure-Sensitive Paint Application to an Oscillating Shock Wave in a Transonic Flow-Reference-Cited by-同舟云学术

Pressure-Sensitive Paint Application to an Oscillating Shock Wave in a Transonic Flow

Published:2015-11 Issue:11 Volume:53 Page:3208-3220
ISSN:0001-1452
Container-title:AIAA Journal
language:en
Short-container-title:AIAA Journal

Author:

Merienne M.-C.¹,Molton P.¹,Bur R.¹,Le Sant Y.¹

Affiliation:

1. Fundamental and Experimental Aerodynamics Department, ONERA–The French Aerospace Lab, 92190 Meudon, France

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Aerospace Engineering

Link

http://arc.aiaa.org/doi/pdf/10.2514/1.J053744

Reference23 articles.

1. LiuT.SullivanJ. P., Pressure and Temperature Sensitive Paint, Springer–Verlag, New York, 2005, pp. 201–262.

2. SURFACE PRESSURE MEASUREMENTS USING LUMINESCENT COATINGS

3. ScrogginA. “Processing an Optimization of Doped Polymer/Ceramic Composite for Luminescent-Based Pressure and Temperature in Aerodynamic Application,” Ph.D. Dissertation, Purdue Univ., West Lafayette, IN, 1999.

4. Porous Pressure-Sensitive Paint for Measurement of Unsteady Pressures in Turbomachinery

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