Analysis for compressible 2-dimensional mixing of 2 reacting gases subjected to steamwise pressure gradient is applicable to limiting cases of frozen or equilibrium flows under assumptions of unit Prandtl and Lewis numbers; empirical law for gas behavior within mixing region is assumed which matches proper density values at points across shear layer; similar solutions of governing system of equations are obtained for various pressure gradients and velocity ratios of 2 reactive streams; applicability to advanced air-breathing vehicles utilizing supersonic combustion.
Similar solutions for laminar mixing of reactive gases
AIAA J
AIAA Journal ; 2 , n 8
1964
7 pages
Article (Journal)
English
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Further similar laminar-flow solutions.
AIAA | 1969
|rratum: Further Similar Laminar-Flow Solutions""
AIAA | 1969
|Turbulent mixing of reactive gases
AIAA | 1965
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