Design of suction slots

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dc.contributor.author A. Fage en_US
dc.contributor.author R. F. Sargent en_US
dc.date.accessioned 2014-10-21T15:50:14Z
dc.date.available 2014-10-21T15:50:14Z
dc.date.issued 1944 en_US
dc.identifier.other ARC/R&M-2127 en_US
dc.identifier.uri https://reports.aerade.cranfield.ac.uk/handle/1826.2/2899
dc.description.abstract Boundary-layer suction is likely to have important applications in the future, particularly on jet-driven low-drag aircraft and in the design of cooling systems. Information will then be needed on the optimum entry shape of two-dimensional slots suitable for boundary-layer suction. The present work, presented in Parts I and II, has been undertaken to obtain such information. en_US
dc.relation.ispartofseries Aeronautical Research Council Reports & Memoranda en_US
dc.title Design of suction slots en_US


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