Correction: Hypervelocity boundary-layer flow with high-temperature surface ablation

Please use this identifier to cite or link to this item: https://doi.org/10.2514/6.2019-3135.c1

DC Field	Value
dc.title	Correction: Hypervelocity boundary-layer flow with high-temperature surface ablation
dc.contributor.author	Temme, Nils
dc.contributor.author	James, Christopher M
dc.contributor.author	McIntyre, Timothy
dc.contributor.author	Lewis, Steven W
dc.contributor.author	Morgan, Richard G
dc.contributor.author	Thirukumaran Nadesan
dc.date.accessioned	2020-07-28T06:33:35Z
dc.date.available	2020-07-28T06:33:35Z
dc.date.issued	2019-06-17
dc.identifier.citation	Temme, Nils, James, Christopher M, McIntyre, Timothy, Lewis, Steven W, Morgan, Richard G, Thirukumaran Nadesan (2019-06-17). Correction: Hypervelocity boundary-layer flow with high-temperature surface ablation. AIAA Aviation 2019 Forum. ScholarBank@NUS Repository. https://doi.org/10.2514/6.2019-3135.c1
dc.identifier.uri	https://scholarbank.nus.edu.sg/handle/10635/171768
dc.publisher	American Institute of Aeronautics and Astronautics
dc.source	Elements
dc.type	Conference Paper
dc.date.updated	2020-07-28T02:49:27Z
dc.contributor.department	MECHANICAL ENGINEERING
dc.description.doi	10.2514/6.2019-3135.c1
dc.description.sourcetitle	AIAA Aviation 2019 Forum
dc.published.state	Published
Appears in Collections:	Staff Publications Elements

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