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- W4308202365 abstract "AbstractAerospike Nozzles (ANs) or altitude compensating nozzles have been under research and development for the Single Stage to Orbit (SSTO) launching vehicles since the 1950s. Plug nozzles are variants of the Aerospike Nozzle (AN) which are truncated along the length. Computational Fluid Dynamics analysis was employed to study the effect of truncation on an AN, with different percentages of truncations such as 0, 20, 40, 60 and 80% of the length of nozzle. For designing the aforesaid AN geometries with different percentages of truncations, Autodesk Fusion 360 software was used. The behaviour of the flow and study of other parameters like velocity, Mach number and temperature were analysed using Ansys Fluent 19.1 software. The analysis was done using the K-Epsilon (k-ε) turbulence model. It is one of the most widely used turbulent analysis models. It has been observed that due to the change in the truncation of the nozzle, we see that the above-stated parameters differ in each case. It is found that the nozzle profile with 40% truncation exhibits superlative results compared to the other nozzle profiles.KeywordsAerospike nozzlePlug nozzlesAltitude compensating nozzleSingle stage to orbit (SSTO)Computational fluid analysisK-epsilon" @default.
- W4308202365 created "2022-11-09" @default.
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- W4308202365 date "2022-11-05" @default.
- W4308202365 modified "2023-09-27" @default.
- W4308202365 title "Influence of Truncation on the Performance of Aerospike Nozzles Using Numerical Technique" @default.
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- W4308202365 doi "https://doi.org/10.1007/978-981-19-3498-8_21" @default.
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