Calculated and experimentally determined explosion pressure ratios obtained in combustion chamber presented over range of fuel air ratios; effects investigated; values of jet thrust and thrust specific fuel consumption obtained from this combustion chamber.
Analytical and experimental performance of explosion-cycle combustion chamber for jet-propulsion engine
Nat Advisory Committee Aeronautics -- Tech Note
1948
59 pages
Report
English
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Structurally Compliant Rocket Engine Combustion Chamber -- Experimental and Analytical Validation
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