Aiaa Aviation 2021 Forum 2021
DOI: 10.2514/6.2021-2966.c1
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Correction: CFD Analysis of Space Launch System Solid Rocket Booster Separation within the Langley Unitary Plan Wind Tunnel

Abstract: The third sentence of the last paragraph in the Conclusion should read: "If the BSMs of a database case were off, solutions required on average 240 SBUs on a 358 million point grid, while if they were on, the consecutive BSMs and test article simulations required on average 15 and 800 SBUs on 30 and 358 million point grids, respectively.", changing the number of SBUs required for a LAVA SLS aero simulation with BSMs on from 240 to 800 (240 is for BSMs off only).

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