Application of pressure sensitive paint to confined flow at mach number 2.5

33rd Joint Propulsion Conference and Exhibit

Volumn , Issue , 1997, Pages

  Lepicovsky, J ^a   Bencic, T C ^b   Bruckner, R J ^b  

^a NASA HEADQUARTERS   (United States)

^b NASA GLENN RESEARCH CENTER   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

AERODYNAMICS; CALIBRATION; LUMINOUS PAINT; MACH NUMBER; PAINT; PRESSURE DISTRIBUTION; PROPULSION; SUPERSONIC AERODYNAMICS; TEMPERATURE;

CALIBRATION PROCEDURE; EFFECTS OF TEMPERATURE; EXTERNAL AERODYNAMICS; INTERNAL REFLECTIONS; NONUNIFORM TEMPERATURE; PRESSURE SENSITIVE PAINTS; STATIC PRESSURE DISTRIBUTIONS; WALL-PRESSURE DISTRIBUTION;

WALL FLOW;

EID: 84962878020     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Conference Paper

References (8)

1. Bruckner, R.J. and Lepicovsky, J.: "A Supersonic Tunnel for Laser and Flow Seeding Techniques", NASA TM-106588, 1994; also AIAA Paper 94-1824, 1994
2. Lepicovsky, J. and Bruckner, R.J.: "Seeding for Laser Velocimetry in Confined Supersonic Flows with Shocks", NASA TM-107265, 1996
3. 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", Paper AIAA 92-0264, 1992
4. Crites R.C.: "Pressure Sensitive Paint Technique", VKI Lecture Series, VKI LS 1993-05, 1993
5. Bencic, T.J.: "Experience Using Pressure Sensitive Paint in NASA Lewis Research Center Propulsion Test Facilities", Paper AIAA 95-2831, 1995
6. Lepicovsky, J., Bruckner, R.J., Bencic, T.J., and Braunscheidel, E.P.: "Modern Experimental Techniques in Turbine Engine Testing", NASA TM-107383, 1996
7. Lepicovsky, J., Schodl, R., and Bruckner, R.J.: "Evaluation of NASA/DLR test Channel for Optical Diagnostic Studies", NASA TM-107507, 1997
8. Morris, M.J. and Donovan, J.F.: "Application of Pressure- and Temperature-Sensitive Paints to High- Speed Flows", Paper AIAA 94-2231, 1994