Acoustic Sensitivities of Lean-Premixed Fuel Injectors in a Single Nozzle Rig
Author:
Affiliation:
1. United Technologies Research Center, Aeromechanical, Chemical, and Fluid Systems, 411 Silver Lane, MS 129-16, East Hartford, CT 06108
2. Pratt & Whitney, 400 Main St., MS 163-16, East Hartford, CT 06108
Abstract
Publisher
ASME International
Subject
Mechanical Engineering,Energy Engineering and Power Technology,Aerospace Engineering,Fuel Technology,Nuclear Energy and Engineering
Link
http://asmedigitalcollection.asme.org/gasturbinespower/article-pdf/121/3/429/5889640/429_1.pdf
Reference20 articles.
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2. Dibble, R. W., Long, M. B., and Masri, A., 1986, “Two-Dimensional Imaging of C2 in Turbulent Nonpremixed Jet Flames,” Dynamics of Reactive Systems: Part II—Modeling and Heterogenous Combustion, Progress in Aeronautics and Astronautics, AIAA, Vol. 105, pp. 99–109.
3. Diederichsen J. , and GouldR., 1965, “Combustion Instability: Radiation from Premixed Flames of Variable Burning Velocity,” Combustion and Flame, Vol. 9, pp. 25–31.
4. Grillo A. , and SlackM., 1976, “Shock Tube Study of Ignition Delay Times in Methane-Oxygen-Nitrogen-Argon Mixtures,” Combustion and Flame, Vol. 27, pp. 377–381.
5. Hurle I. , PriceR., SugdenT., and ThomasA., 1968, “Sound From Open Turbulent Premixed Flames,” Proc. Roy. Soc., Vol. 303, pp. 409–427.
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