scholarly journals Data Processing of Pressure-Sensitive Paint in JAXA Industrial Wind Tunnel

2006 ◽  
Vol 26 (Supplement1) ◽  
pp. 211-214 ◽  
Author(s):  
Mitsuru KURITA ◽  
Kazunori MITSUO ◽  
Shigeru KUCHIISHI ◽  
Kazuyuki NAKAKITA ◽  
Shigeya WATANABE ◽  
...  
Keyword(s):  
Wind Tunnel ◽  
Data Processing ◽  
Pressure Sensitive Paint ◽  
Pressure Sensitive

Automatic Data Processing of Pressure-Sensitive Paint Measurement in a Wind Tunnel

2014 ◽  
Author(s):  
Mitsuru Kurita ◽  
Kazuyuki Nakakita ◽  
Kazunori Mitsuo ◽  
Hideki Yamaya ◽  
Tsutomu Nakajima
Keyword(s):  
Wind Tunnel ◽  
Data Processing ◽  
Automatic Data Processing ◽  
Pressure Sensitive Paint ◽  
Automatic Data ◽  
Pressure Sensitive

Data Processing Methods for Unsteady Pressure-Sensitive Paint Application

2018 ◽  
Author(s):  
Nettie Roozeboom ◽  
Christina Ngo ◽  
Jessica M. Powell ◽  
Jennifer Baerny ◽  
David Murakami ◽  
...  
Keyword(s):  
Data Processing ◽  
Pressure Sensitive Paint ◽  
Processing Methods ◽  
Unsteady Pressure ◽  
Pressure Sensitive ◽  
Data Processing Methods

The Application of Pressure- and Temperature-Sensitive Paints to an Advanced Compressor

2000 ◽  
Vol 123 (4) ◽  
pp. 823-829 ◽  
Author(s):  
Kelly R. Navarra ◽  
Douglas C. Rabe ◽  
Sergey D. Fonov ◽  
Larry P. Goss ◽  
Chunill Hah
Keyword(s):  
Wind Tunnel ◽  
Molecular Spectroscopy ◽  
State Of The Art ◽  
Temperature Sensitive ◽  
Pressure Sensitive Paint ◽  
Suction Surface ◽  
Transonic Compressor ◽  
Pressure Sensitive ◽  
Oxygen Sensitive ◽  
Design Speed

An innovative pressure-measurement technique that employs the tools of molecular spectroscopy has been widely investigated by the aerospace community. Measurements are made via oxygen-sensitive molecules attached to the surface of interest as a coating, or paint. The pressure-sensitive-paint (PSP) technique is now commonly used in stationary wind-tunnel tests; this paper presents the use of this technique in advanced turbomachinery applications. New pressure- and temperature-sensitive paints (P/TSPs) have been developed for application to a state-of-the-art transonic compressor where pressures up to 1.4 atm and surface temperatures to 90°C are expected for the suction surface of the first-stage rotor. PSP and TSP data images have been acquired from the suction surface of the first-stage rotor at 85 percent of the corrected design speed for the compressor near-stall condition. A comparison of experimental results with CFD calculations is discussed.

Sign in / Sign up

Export Citation Format

Share Document