The application of pressure- and temperature-sensitive paints to an advanced compressor

Journal of Turbomachinery

Volumn 123, Issue 4, 2001, Pages 823-829

  Navarra, K R ^a   Rabe, D C ^a   Fonov, S D ^a   Goss, L P ^a   Hah, C ^a  

^a AIR FORCE RESEARCH LABORATORY   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

COMPRESSORS; COMPUTATIONAL FLUID DYNAMICS; IMAGE ANALYSIS; ROTORS; TRANSONIC FLOW; WIND TUNNELS;

PRESSURE SENSITIVE PAINTS (PSP); TEMPERATURE SENSITIVE PAINTS (TSP);

PAINT;

COMPUTATIONAL FLUID DYNAMICS; GAS TURBINE; PAINT; TURBOMACHINERY;

EID: 0035483452     PISSN: 0889504X     EISSN: None     Source Type: Journal    
DOI: 10.1115/1.1400116     Document Type: Article

References (21)

1. Pressure-sensitive-paint measurements in a large-scale commercial-engine test stand
2. Optical measurements of surface pressure and temperature in turbomachinery
3. Pressure-sensitive paint investigation for application in turbomachinery
4. Rotor blade pressure measurement in a high speed axial compressor using pressure and temperature sensitive paints
5. Rotating pressure and temperature measurements-on scale-model fans using luminescent paints
6. Luminescence barometry in wind tunnels
7. Aerodynamic applications of pressure sensitive paint
8. Pressure-sensitive paint in aerodynamic testing
9. Temperature- and pressure-sensitive luminescent paints in aerodynamics
10. Surface pressure measurements in supersonic transverse injection flowfields
11. Sol-Gel-Based pressure-sensitive paint development
12. Tip flow fields in a low aspect ratio transonic compressor
13. Data analysis techniques for pressure- and temperature-sensitive paint
14. Image registration for luminescent paint sensors
15. Data-Analysis methods for the development and deployment of pressure-sensitive paints
16. Effects of inlet distortion on the flow field in a transonic compressor rotor
17. Three-Dimensional flowfields inside a transonic compressor with swept blades