Busemann correction to the characteristics of the two-dimensional hypersonic sail

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dc.contributor.authorBoyd, E. A.
dc.date.accessioned2014-11-25T17:38:53Z
dc.date.available2014-11-25T17:38:53Z
dc.date.issued1960-11
dc.description.abstractThe two-dimensional hypersonic sail is examined using the Newton- Busemann pressure law. The results are compared with those of Daskin and Feldman (1958) who used the empirical modified Newtonian pressure law. It is found that for a given chord length of sail a corrected sail will give a specified lift for a smaller tension in the sail. At a flight Mach number of 10 at 100,000 ft. the tension in one particular sail considered could be supported with a working stress of about 20 tons/in[squared].en_UK
dc.identifier.urihttp://dspace.lib.cranfield.ac.uk/handle/1826/8815
dc.language.isoenen_UK
dc.publisherCollege of Aeronauticsen_UK
dc.relation.ispartofseriesCollege of Aeronautics Reportsen_UK
dc.relation.ispartofseries140en_UK
dc.relation.ispartofseriesCOA/140en_UK
dc.titleBusemann correction to the characteristics of the two-dimensional hypersonic sailen_UK
dc.typeReporten_UK

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