A review of pressure-sensitive paint for high-speed and unsteady aerodynamics-Reference-Cited by-同舟云学术

A review of pressure-sensitive paint for high-speed and unsteady aerodynamics

Published:2008-02-01 Issue:2 Volume:222 Page:249-290
ISSN:0954-4100
Container-title:Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering
language:en
Short-container-title:Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering

Author:

Gregory J W¹,Asai K²,Kameda M³,Liu T⁴,Sullivan J P⁵

Affiliation:

1. Department of Aerospace Engineering, The Ohio State University, Ohio, USA

2. Department of Aerospace Engineering, Graduate School of Engineering, Tohoku University, Aoba-ku, Sendai, Japan

3. Department of Mechanical Systems Engineering, Tokyo University of Agriculture and Technology, Koganei, Tokyo, Japan

4. Applied Aerodynamics Laboratory, Department of Mechanical and Aeronautical Engineering, College of Engineering and Applied Sciences, Western Michigan University, Kalamazoo, Michigan, USA

5. Department of Aeronautics and Astronautics, Purdue University, West Lafayette, Indiana, USA

Abstract

The current paper describes the development of pressure-sensitive paint (PSP) technology as an advanced measurement technique for unsteady flow fields and short-duration wind tunnels. Newly developed paint formulations have step response times approaching 1 μs, making them suitable for a wide range of unsteady testing. Developments in binder technology are discussed, which have resulted in new binder formulations such as anodized aluminium, thin-layer chromatography plate, polymer/ceramic, and poly(TMSP) PSP. The current paper also details modeling work done to describe the gas diffusion properties within the paint binder and understand the limitations of the paint response characteristics. Various dynamic calibration techniques for PSP are discussed, along with summaries of typical response times. A review of unsteady and high-speed PSP applications is presented, including experiments with shock tubes, hypersonic tunnels, unsteady delta wing aerodynamics, fluidic oscillator flows, Hartmann tube oscillations, acoustics, and turbomachinery. Flowfields with fundamental frequencies as high as 21 kHz have been successfully measured with porous PSP formulations.

Publisher

SAGE Publications

Subject

Mechanical Engineering,Aerospace Engineering

Link

http://journals.sagepub.com/doi/pdf/10.1243/09544100JAERO243

Reference93 articles.

1. Luminescent barometry in wind tunnels

2. Temperature- and Pressure-Sensitive Luminescent Paints in Aerodynamics

3. SURFACE PRESSURE MEASUREMENTS USING LUMINESCENT COATINGS

4. Optimum Thickness of Pressure-Sensitive Paint for Unsteady Measurements

Cited by 333 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. High-Bandwidth Pressure Field Imaging of Stream-Traced Inlet Unstart Dynamics;AIAA Journal;2024-09-12

2. Pressure-Sensitive-Paint-Driven Hybrid Unsteady Compressible Flow Simulation;AIAA Journal;2024-09-02

3. Resolving high-frequency aeroacoustic noises of high-speed dual-impinging jets using fast pressure-sensitive paint;Experiments in Fluids;2024-08-26

4. Triple decomposition and sparse representation for noisy pressure-sensitive paint data;Physics of Fluids;2024-07-01

5. Dynamics of a 3-D inlet/isolator measured with fast pressure-sensitive paint;Experiments in Fluids;2024-07