Predicted Mass-Fraction and Concentration Distributions for Subsonic Turbulent Mixing Flow Based on Stagnation and Static Pressure and Temperature Measurements
Author:
Affiliation:
1. Hampton University
2. Institute for Aerospace Studies, University of Toronto
3. NASA Glenn Research Center
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.2009-4048
Reference7 articles.
1. Gonor, A.L., Khaikine, V.A.,Gottlieb, J.J., andBlankson, I.M.,2008, Method for Determinationofthe Injectant and Species Mass Fractions and Concentration Distributions in Supersonic Turbulent Mixing witha Multi-Species Co-Flow, AIAApaper 2008-2656.
2. Gonor, A.L., Khaikine, V.A., Gottlieb, J.J., and Blankson, I.M., 2006, An Accurate Experimental Method for Determining the Injectant Mass Fraction Distribution in a Supersonic Turbulent Flow MixingRegion,AIAApaper2006-8147.
3. Gonor, A.L., Khaikine, V.A., Gottlieb, J.J., and Blankson, I.M., 2006, An Accurate Method for Determining the Injectant Mass Fraction Distribution in a Scramjet Engine Channel and Influence of the Mixing Efficiency on Performance of the Engine and Pylon Set Located in the Inlet, AIAA paper 2006-4917.
4. Computational Study of the Propulsive Characteristics of a Shcramjet Engine
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1. Determining the Hydrogen Mass Fraction, Concentration Distributions and Related Flow Properties in a Subsonic Turbulent Mixing Region with a Multi-Species Co-Flow;40th Fluid Dynamics Conference and Exhibit;2010-06-28
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