{"comment":{"created_at":"2011-10-19T21:54:10Z","body":"Florian,\r\n\r\nI have corrected this now. See new commit to OP2-Common\r\n\r\nThe problem was just a matter of replacing the doubles in airfoil.cpp to floats.\r\nProbably caused by the fact that Carlo and myself copied the DP directory\r\nthat day to an SP directory and forgot to update the sequential airfoil version to\r\nsingle precision. \r\n\r\nLet me know if this there are any further errors.\r\n\r\nThanks,\r\n\r\nGihan \r\n\r\n-----------------------------------------------------------------\r\n  Dr. Gihan R. Mudalige\r\n  Research Associate\r\n  Oxford e-Research Centre,\r\n  University of Oxford,\r\n  7 Keble Road,\r\n  Oxford. OX1 3QG\r\n  Tel: +44 (0)1865 610787\r\n  Email: gihan.mudalige@oerc.ox.ac.uk\r\n-----------------------------------------------------------------\r\n________________________________________\r\nFrom: Florian Rathgeber [reply@reply.github.com]\r\nSent: 19 October 2011 18:35\r\nTo: Gihan Mudalige\r\nSubject: [OP2-Common] airfoil_seq single precision does not converge (C) (#6)\r\n\r\n```\r\n 100  1.71585e-160\r\n 200  1.71585e-160\r\n 300  1.71585e-160\r\n 400  1.71585e-160\r\n 500  1.71585e-160\r\n 600  1.71585e-160\r\n 700  1.71585e-160\r\n 800  1.71585e-160\r\n 900  1.71585e-160\r\n 1000  1.71585e-160\r\n```\r\n\r\n--\r\nReply to this email directly or view it on GitHub:\r\nhttps://github.com/carlobertolli/OP2-Common/issues/6","updated_at":"2011-10-19T21:54:10Z","url":"https://api.github.com/repos/carlobertolli/OP2-Common/issues/comments/2461765","id":2461765,"user":{"avatar_url":"https://secure.gravatar.com/avatar/751d9453187d339e2de8eddf624fca19?d=https://a248.e.akamai.net/assets.github.com%2Fimages%2Fgravatars%2Fgravatar-140.png","gravatar_id":"751d9453187d339e2de8eddf624fca19","url":"https://api.github.com/users/gihanmudalige","id":674680,"login":"gihanmudalige"}},"action":"created","issue":{"number":6,"created_at":"2011-10-19T17:35:18Z","pull_request":{"diff_url":null,"patch_url":null,"html_url":null},"body":"```\r\n 100  1.71585e-160\r\n 200  1.71585e-160\r\n 300  1.71585e-160\r\n 400  1.71585e-160\r\n 500  1.71585e-160\r\n 600  1.71585e-160\r\n 700  1.71585e-160\r\n 800  1.71585e-160\r\n 900  1.71585e-160\r\n 1000  1.71585e-160\r\n```","comments":1,"title":"airfoil_seq single precision does not converge (C)","updated_at":"2011-10-19T21:54:10Z","url":"https://api.github.com/repos/carlobertolli/OP2-Common/issues/6","id":1996344,"assignee":null,"milestone":null,"closed_at":null,"user":{"avatar_url":"https://secure.gravatar.com/avatar/d178a6201be696c466c41c355c671707?d=https://a248.e.akamai.net/assets.github.com%2Fimages%2Fgravatars%2Fgravatar-140.png","gravatar_id":"d178a6201be696c466c41c355c671707","url":"https://api.github.com/users/kynan","id":346079,"login":"kynan"},"html_url":"https://github.com/carlobertolli/OP2-Common/issues/6","labels":[{"name":"C","url":"https://api.github.com/repos/carlobertolli/OP2-Common/labels/C","color":"444444"}],"state":"open"},"legacy":{"issue_id":1996344,"comment_id":2461765}}