dc.contributor.author | T. A. Cook | en_US |
dc.date.accessioned | 2014-10-20T11:03:59Z | |
dc.date.available | 2014-10-20T11:03:59Z | |
dc.date.issued | 1965 | en_US |
dc.identifier.other | ARC/CP-804 | en_US |
dc.identifier.uri | https://reports.aerade.cranfield.ac.uk/handle/1826.2/817 | |
dc.relation.ispartofseries | Aeronautical Research Council Current Papers | en_US |
dc.title | Wind tunnel tests at mach numbers up to 2.80 to determine the effects of changing spanwise volume distribution on a slender, cambered ogee wing | en_US |