A laser-induced incandescence system for measuring soot flux in aircraft engine exhausts

38th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit

Volumn , Issue , 2002, Pages

  Jenkins, T P ^a   Bartholomew, J L ^a   DeBarber, P A ^a   Yang, P ^b   Seitzman, J M ^b   Howard, R P ^c  

^a METROLASER INC   (United States)

^b GEORGIA INSTITUTE OF TECHNOLOGY   (United States)

^c JACOBS TECHNOLOGY   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

LABORATORY EXPERIMENTS; LASER INDUCED INCANDESCENCE; MEASUREMENTS OF; NON-INTRUSIVE MEASUREMENTS; PARTICLE SIZING; RAPID MEASUREMENT; SOOT CONCENTRATION; SPATIAL RESOLUTION;

DUST; EXHAUST SYSTEMS (ENGINE); PARTICLE SIZE; PROPULSION; SOOT;

AIRCRAFT ENGINES;

EID: 84896866867     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Conference Paper

References (13)

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8. Schfer, K, Heland, J, Lister, D. H., et al., "Nonintrusive Optical Measurements of Aircraft Engine Exhaust Emissions and Comparison with Standard Intrusive Techniques, " Appl. Optics 39, 441 (2000).
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13. Jenkins, T. P., Bartholomew, J. L., and DeBarber, P. A., "A Real-Time Non-Intrusive Measurement System for Soot Properties in Aircraft Engine Exhausts, " Final Report, USAF contract F40600-98-C-0014 (2002).