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For one - dimensional chambered flame, ( i ) provide detailed derivation to show t i l d e ( T ) f - t
For onedimensional chambered flame, i provide detailed derivation to show
ii compute the mass fluxes of fuel, oxidizer, and product at and ; ii based on the mass fluxes of fuel and oxidizer at the boundaries, determine the equivalence ratio of the combustion system in terms of tilde and tilde; iii determine the net thrust per unit area generated by the combustion chamber, assuming and are nonzero.
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