Two-component laser anemometry measurements of non-reacting and reacting complex flows in a swirl-stabilized model combustor

Author:

Brum R. D.,Samuelsen G. S.

Publisher

Springer Science and Business Media LLC

Subject

Fluid Flow and Transfer Processes,General Physics and Astronomy,Mechanics of Materials,Computational Mechanics

Reference15 articles.

1. Brum, R. D.; Samuelsen, G. S. 1982 a: Two-component laser anemometry measurements in a non-reacting and reacting complex flow model combustor. Presented at the 1982 Fall Meeting, Western States Section/The Combustion Institute, Livermore CA, USA

2. Brum, R. D.; Samuelsen, G. S. 1982b: Assessment of a dilute swirl combustor as a bench scale, complex flow test bed for modeling, diagnostics, and fuels effects studies. AIAA Paper 82-1263

3. Brum, R. D. 1983: Detailed data set: two-color laser anemometry measurements of non-reacting and reacting flows in the dilute swirl combustor. UCI-ARTR-83-10, UCI Combustion Laboratory, Mechanical Engineering, University of California, Irvine CA, USA

4. Cheng, R. K. 1984: Conditioned sampling of turbulence intensities and Reynolds stress in premixed turbulent flames. Combust. Sci. Technol. 41, 109?142

5. Dils, R. R. 1973: Dynamic gas temperature measurements in a gas turbine transition duet exit. J. Eng. Power 95, 265?277

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