Charts presented apply to processes in which final mixture is leaner than stoichiometric and are exact below those temperatures at which dissociation becomes important; need arises in performance analysis of aircraft gas turbine engines when diluents or refrigerants are used to augment thrust or power of engine. (25¢)
Constant-pressure combustion on charts including effects of diluent addition
Nat Advisory Committee Aeronautics -- Report
1949
25 pages
Report
English
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