Application of DPIV to enhanced mixing heated nozzle flows

40th AIAA Aerospace Sciences Meeting and Exhibit

Volumn , Issue , 2002, Pages

  Wernet, Mark P ^a   Bridges, James ^a  

^a NASA GLENN RESEARCH CENTER   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

EID: 84894386323     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Conference Paper

References (5)

1. Castner, R. S., 1994 "The Nozzle Acoustic Test Rig: An Acoustic and Aerodynamic Free-Jet Facility", NASA TM 106495.
2. Janardan, B.A., Hoff, G.E., Baiter, J.W., Martens, S., Gliebe, P.R., Mengle, V., and Dalton, W.N., 2000 "AST Critical Propulsion and Noise Reduction Technologies for Future Commercial Subsonic Engines Separate-Row Exhaust System Noise Reduction Concept Evaluation, " NASA CR 2000-210039.
3. Saiyed, N., ed., 2000 "Separate Flow Nozzle Test Status Meeting", NASA CP 2000-210524.
4. Saiyed, N., Mikkelsen, K.L., and Bridges, J., 2000 "Acoustics and Thrust of Separate-Row Exhaust Nozzles With Mixing Devices for High-Bypass-Ratio Engines", NASA TM 2000-209948.
5. Wernet, M. P., 1999 "Fuzzy Logic Enhanced Digital PIV Processing Software", Proceedings of the 18th International Congress on Instrumentation for Aerospace Simulation Facilities (ICIASF), Toulouse, France.