Computational Study on the Flow Characteristics in a Film Cooled Dual-Bell Nozzle
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Publisher
Springer Singapore
Link
http://link.springer.com/content/pdf/10.1007/978-981-15-5183-3_24
Reference12 articles.
1. Foster C, Cowles F (1949) Experimental study of gas-flow separation in over expanded exhaust nozzles for rocket motors. Jet Propulsion Lab Progress Report, 4-103
2. Horn M, Fisher S (1994) Dual-bell altitude compensating nozzles. NASA CR-194719
3. Nasuti F, Onofri M, Martelli E (2005) Role of wall shape on the transition in dual-bell nozzles. J Propulsion Power 21(2):243–250
4. Martelli E, Nasuti F, Onofri M (2007) Numerical parametric analysis of dual-bell nozzle flows. AIAA J 45(3):640–650
5. Génin C, Stark R (2011) Experimental investigation of the inflection geometry on dual bell nozzle flow behavior. In: 47th AIAA/ASME/SAE/ASEE joint propulsion conference & exhibit, 31 July–03 August
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1. Computational investigation of cooling effectiveness for film cooled dual-bell exhaust nozzle for LO2/LH2 liquid rocket engines;Energy Sources, Part A: Recovery, Utilization, and Environmental Effects;2021-09-04
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