{"id":30,"date":"2012-04-08T20:47:00","date_gmt":"2012-04-09T01:47:00","guid":{"rendered":"http:\/\/charles-oneill.com\/blog\/?p=30"},"modified":"2014-07-31T11:17:08","modified_gmt":"2014-07-31T16:17:08","slug":"presentation-aircraft-flight-dynamics-with-a-non-inertial-cfd-code","status":"publish","type":"post","link":"https:\/\/charles-oneill.com\/blog\/presentation-aircraft-flight-dynamics-with-a-non-inertial-cfd-code\/","title":{"rendered":"Presentation: Aircraft Flight Dynamics with a Non-Inertial CFD Code"},"content":{"rendered":"<div style=\"text-align: center;\">Aircraft Flight Dynamics with a Non-Inertial CFD Code<\/div>\n<div style=\"text-align: center;\"><span style=\"background-color: white;\">AIAA 2005-0230<\/span><\/div>\n<div style=\"text-align: center;\"><\/div>\n<div style=\"text-align: center;\">Charles O&#8217;Neill<\/div>\n<div style=\"text-align: center;\">Jan 2005<\/div>\n<div style=\"text-align: center;\">Reno, NV<\/div>\n<p><\/p>\n<div style=\"text-align: left;\">This project was presented as&nbsp;<span style=\"background-color: white; text-align: center;\">AIAA 2005-0230 and concerns coupling a non-inertial CFD code with a 6 DOF (degree of freedom) rigid body dynamics simulator. Quaternions are used for attitude orientation. The result is a&nbsp;computational&nbsp;aircraft flight dynamics simulation. The paper shows flight maneuvers such as rolls, loops, and thin-strip Magnus lift production.<\/span><\/div>\n<table align=\"center\" cellpadding=\"0\" cellspacing=\"0\" style=\"margin-left: auto; margin-right: auto; text-align: center;\">\n<tbody>\n<tr>\n<td style=\"text-align: center;\"><a href=\"http:\/\/charles-oneill.com\/blog\/wp-content\/uploads\/2012\/04\/navion_roll.png\" style=\"margin-left: auto; margin-right: auto; text-align: center;\"><img loading=\"lazy\" decoding=\"async\" border=\"0\" height=\"196\" src=\"http:\/\/charles-oneill.com\/blog\/wp-content\/uploads\/2012\/04\/navion_roll-300x184.png\" width=\"320\" \/><\/a><\/td>\n<\/tr>\n<tr>\n<td style=\"text-align: center;\">Navion Roll with Rudder Deflection<\/td>\n<\/tr>\n<\/tbody>\n<\/table>\n<p>The full presentation is available&nbsp;<a href=\"http:\/\/charles-oneill.com\/projects\/reno05_AIAA2005_0230.pdf\">here<\/a>.<\/p>\n","protected":false},"excerpt":{"rendered":"<p>Aircraft Flight Dynamics with a Non-Inertial CFD Code AIAA 2005-0230 Charles O&#8217;Neill Jan 2005 Reno, NV This project was presented as&nbsp;AIAA 2005-0230 and concerns coupling a non-inertial CFD code with a 6 DOF (degree of freedom) rigid body dynamics simulator. Quaternions are used for attitude orientation. The result is a&nbsp;computational&nbsp;aircraft flight dynamics simulation. The paper [&hellip;]<\/p>\n","protected":false},"author":1,"featured_media":61,"comment_status":"open","ping_status":"open","sticky":false,"template":"","format":"standard","meta":{"footnotes":""},"categories":[1],"tags":[],"_links":{"self":[{"href":"https:\/\/charles-oneill.com\/blog\/wp-json\/wp\/v2\/posts\/30"}],"collection":[{"href":"https:\/\/charles-oneill.com\/blog\/wp-json\/wp\/v2\/posts"}],"about":[{"href":"https:\/\/charles-oneill.com\/blog\/wp-json\/wp\/v2\/types\/post"}],"author":[{"embeddable":true,"href":"https:\/\/charles-oneill.com\/blog\/wp-json\/wp\/v2\/users\/1"}],"replies":[{"embeddable":true,"href":"https:\/\/charles-oneill.com\/blog\/wp-json\/wp\/v2\/comments?post=30"}],"version-history":[{"count":0,"href":"https:\/\/charles-oneill.com\/blog\/wp-json\/wp\/v2\/posts\/30\/revisions"}],"wp:featuredmedia":[{"embeddable":true,"href":"https:\/\/charles-oneill.com\/blog\/wp-json\/wp\/v2\/media\/61"}],"wp:attachment":[{"href":"https:\/\/charles-oneill.com\/blog\/wp-json\/wp\/v2\/media?parent=30"}],"wp:term":[{"taxonomy":"category","embeddable":true,"href":"https:\/\/charles-oneill.com\/blog\/wp-json\/wp\/v2\/categories?post=30"},{"taxonomy":"post_tag","embeddable":true,"href":"https:\/\/charles-oneill.com\/blog\/wp-json\/wp\/v2\/tags?post=30"}],"curies":[{"name":"wp","href":"https:\/\/api.w.org\/{rel}","templated":true}]}}