{"action":"created","issue":{"url":"https://api.github.com/repos/Tudat/tudat/issues/91","repository_url":"https://api.github.com/repos/Tudat/tudat","labels_url":"https://api.github.com/repos/Tudat/tudat/issues/91/labels{/name}","comments_url":"https://api.github.com/repos/Tudat/tudat/issues/91/comments","events_url":"https://api.github.com/repos/Tudat/tudat/issues/91/events","html_url":"https://github.com/Tudat/tudat/pull/91","id":189746125,"number":91,"title":"Aerothermodynamics functions now included in the Aerodynamics module.","user":{"login":"agzrocket","id":7430977,"avatar_url":"https://avatars.githubusercontent.com/u/7430977?v=3","gravatar_id":"","url":"https://api.github.com/users/agzrocket","html_url":"https://github.com/agzrocket","followers_url":"https://api.github.com/users/agzrocket/followers","following_url":"https://api.github.com/users/agzrocket/following{/other_user}","gists_url":"https://api.github.com/users/agzrocket/gists{/gist_id}","starred_url":"https://api.github.com/users/agzrocket/starred{/owner}{/repo}","subscriptions_url":"https://api.github.com/users/agzrocket/subscriptions","organizations_url":"https://api.github.com/users/agzrocket/orgs","repos_url":"https://api.github.com/users/agzrocket/repos","events_url":"https://api.github.com/users/agzrocket/events{/privacy}","received_events_url":"https://api.github.com/users/agzrocket/received_events","type":"User","site_admin":false},"labels":[],"state":"open","locked":false,"assignee":null,"assignees":[],"milestone":null,"comments":11,"created_at":"2016-11-16T15:51:42Z","updated_at":"2016-11-29T16:21:56Z","closed_at":null,"pull_request":{"url":"https://api.github.com/repos/Tudat/tudat/pulls/91","html_url":"https://github.com/Tudat/tudat/pull/91","diff_url":"https://github.com/Tudat/tudat/pull/91.diff","patch_url":"https://github.com/Tudat/tudat/pull/91.patch"},"body":"First iteration of the aerothermodynamics functions. Only aerodynamic load (aka load factor) and heat flux were added. Heat load should be the integral of the heat flux, so I suppose that should go somewhere else. Cheers"},"comment":{"url":"https://api.github.com/repos/Tudat/tudat/issues/comments/263618441","html_url":"https://github.com/Tudat/tudat/pull/91#issuecomment-263618441","issue_url":"https://api.github.com/repos/Tudat/tudat/issues/91","id":263618441,"user":{"login":"DominicDirkx","id":5039068,"avatar_url":"https://avatars.githubusercontent.com/u/5039068?v=3","gravatar_id":"","url":"https://api.github.com/users/DominicDirkx","html_url":"https://github.com/DominicDirkx","followers_url":"https://api.github.com/users/DominicDirkx/followers","following_url":"https://api.github.com/users/DominicDirkx/following{/other_user}","gists_url":"https://api.github.com/users/DominicDirkx/gists{/gist_id}","starred_url":"https://api.github.com/users/DominicDirkx/starred{/owner}{/repo}","subscriptions_url":"https://api.github.com/users/DominicDirkx/subscriptions","organizations_url":"https://api.github.com/users/DominicDirkx/orgs","repos_url":"https://api.github.com/users/DominicDirkx/repos","events_url":"https://api.github.com/users/DominicDirkx/events{/privacy}","received_events_url":"https://api.github.com/users/DominicDirkx/received_events","type":"User","site_admin":false},"created_at":"2016-11-29T16:21:56Z","updated_at":"2016-11-29T16:21:56Z","body":"Hi Alejandro,\r\n\r\nI've added some unit tests for the heating/equilibrium temperature. I've also added some extra tests for the dependent variable saving and commenting all the new stuff, see my branch:\r\n\r\nhttps://github.com/DominicDirkx/tudat/tree/agzrocket-aerothermodynamics\r\n\r\nCould you check if the code runs properly (e.g. all unit tests pass) on your machine, and give the small changes I've made a quick look? If you're happy with everything, I'll push this to the master,\r\n\r\nCheers,\r\n\r\nDominic"}}
{"actor":{"display_login":"DominicDirkx"}}