Rotating pressure and temperature measurements on scale-model fans using luminescent paints

34th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit

Volumn , Issue , 1998, Pages

  Bencic, Timothy J ^a  

^a NASA GLENN RESEARCH CENTER   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

AERODYNAMICS; DATA ACQUISITION; NASA; PROPULSION; TEMPERATURE DISTRIBUTION; WIND TUNNELS;

DETECTION PROBLEMS; FULL-FIELD MEASUREMENT; ILLUMINATION SOURCES; LOW-SPEED WIND TUNNEL; MEASUREMENT TECHNIQUES; PRESSURE AND TEMPERATURE; TEMPERATURE DEPENDENCE; WIND TUNNEL MEASUREMENTS;

TEMPERATURE MEASUREMENT;

EID: 84963827839     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Conference Paper

References (12)

1. Kavandi, J., Callis, J., Gouterman, M., Khalil, G., Wright, D., Green, E., Burns, D., and McLachlan, B., "Luminescent Barometry in Wind Tunnels", Review of Scientific Instruments, Vol. 61, No. 11, pp. 3340-3347, 1997.
2. Morris, M.J., Donovan, J.F., Kegelman, J.T., Schwab, S.D., Levy, R.L., and Crites, R.C., "Aerodynamic Applications of Pressure Sensitive Paint", AIAA Journal, Vol. 31, No. 3, pp.419-425, 1993.
3. Morris, M.J., Benne, M.E., Crites, R.C., and Donovan, J.F., "Aerodynamic Measurements Based on Photoluminescence", AIAA Paper 93-0175, 1993.
4. McLachlin, B.G. and Bell, J.H., "Pressure Sensitive Paint hi Aerodynamic Testing", Experimental Thermal and Fluid Science, 10, pp. 470-485, 1995.
5. Bencic, T.J., "Experiences Using Pressure Sensitive Paint in NASA Lewis Research Center Test Facilities", AIAA Paper 95-2831, 1995.
6. Lepicovsky, J., Bencic, T.J. and Bruckner, R.J., "Application of Pressure Sensitive Paint to Confined Flow at Mach Number 2.5", AIAA Paper 97-3214, 1997.
7. th Int. Congress on Instrumentation in Aerospace Simulation Facilities, IEEE, Wright Patterson AFB, Dayton, OH, pp.32.1-32.14, 1995.
8. Sabroske, K.R., et al, "Pressure Sensitive Paint Investigation for Application in Turbomachinery", ASME Paper 95-GT-92, 1995.
9. Liu, T., Torgerson, S., Sullivan, J., Johnston, R. and Fleeter, S., "Rotor Blade Measurements in a High Speed Axial Compressor using Pressure and Temperature Sensitive Paints", AIAA Paper 97-0162, 1997.
10. Jordan, J.D., Trump, D.D., Sarka, B., Navarra, K.R., Weaver, W.L. and Goss, L.P., "High-Frequency Pressure Sensitive Paints for Turbomachinery Applications", Proc. of 44th Int. Instrumentation Symposium, ISA Aerospace Test Measurements, pp. 110-119, 1998.
11. Woodmansee, M.A. and Dutton, J.C., "Methods for Treating Temperature Sensitivity Effects of Pressure Sensitive Paints", AIAA Paper 97-0387, 1997.
12. Lepicovsky, J., Bruckner, R.J., Bencic, T.J. and Braunschiedel, E.P., "Modern Experimental Techniques hi Turbine Engine Testing", NASA TM-107383, 1996.