Study, made to evaluate various methods of minimizing overall pressure ratio required to establish and maintain full expansion of nozzle flow, investigating cylindrical diffusers, diffusers with contraction and diffusers including right-angle turn; results obtained are summarized.
Experimental evaluation of rocket exhaust diffusers for altitude simulation
NASA -- Tech Note
1960
43 pages
Report
English
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Investigation of Rocket Exhaust Diffusers for Altitude Simulation
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