{"version":"1.0","provider_name":"Flow Science and Engineering","provider_url":"https:\/\/engineering.jhu.edu\/zaki","title":"Turbomachinery - Flow Science and Engineering","type":"video","width":600,"height":338,"html":"<blockquote class=\"wp-embedded-content\" data-secret=\"emaDb4OkO2\"><a href=\"https:\/\/engineering.jhu.edu\/zaki\/research\/turbomachinery\/\">Turbomachinery<\/a><\/blockquote><iframe sandbox=\"allow-scripts\" security=\"restricted\" src=\"https:\/\/engineering.jhu.edu\/zaki\/research\/turbomachinery\/embed\/#?secret=emaDb4OkO2\" width=\"600\" height=\"338\" title=\"&#8220;Turbomachinery&#8221; &#8212; Flow Science and Engineering\" data-secret=\"emaDb4OkO2\" frameborder=\"0\" marginwidth=\"0\" marginheight=\"0\" scrolling=\"no\" class=\"wp-embedded-content\"><\/iframe><script>\n\/*! This file is auto-generated *\/\n!function(d,l){\"use strict\";l.querySelector&&d.addEventListener&&\"undefined\"!=typeof URL&&(d.wp=d.wp||{},d.wp.receiveEmbedMessage||(d.wp.receiveEmbedMessage=function(e){var t=e.data;if((t||t.secret||t.message||t.value)&&!\/[^a-zA-Z0-9]\/.test(t.secret)){for(var s,r,n,a=l.querySelectorAll('iframe[data-secret=\"'+t.secret+'\"]'),o=l.querySelectorAll('blockquote[data-secret=\"'+t.secret+'\"]'),c=new RegExp(\"^https?:$\",\"i\"),i=0;i<o.length;i++)o[i].style.display=\"none\";for(i=0;i<a.length;i++)s=a[i],e.source===s.contentWindow&&(s.removeAttribute(\"style\"),\"height\"===t.message?(1e3<(r=parseInt(t.value,10))?r=1e3:~~r<200&&(r=200),s.height=r):\"link\"===t.message&&(r=new URL(s.getAttribute(\"src\")),n=new URL(t.value),c.test(n.protocol))&&n.host===r.host&&l.activeElement===s&&(d.top.location.href=t.value))}},d.addEventListener(\"message\",d.wp.receiveEmbedMessage,!1),l.addEventListener(\"DOMContentLoaded\",function(){for(var e,t,s=l.querySelectorAll(\"iframe.wp-embedded-content\"),r=0;r<s.length;r++)(t=(e=s[r]).getAttribute(\"data-secret\"))||(t=Math.random().toString(36).substring(2,12),e.src+=\"#?secret=\"+t,e.setAttribute(\"data-secret\",t)),e.contentWindow.postMessage({message:\"ready\",secret:t},\"*\")},!1)))}(window,document);\n\/\/# sourceURL=https:\/\/engineering.jhu.edu\/zaki\/wp-includes\/js\/wp-embed.min.js\n<\/script>\n","description":"This research collaboration aims at simulating, in detail, the role of transition in compressor aerodynamics.\u00a0The flow through the passage is subjected to adverse pressure gradient, which is destabilizing, and can lead to transition to turbulence or boundary layer separation.\u00a0In addition to the mean pressure gradient, the boundary layers on the compressor blade are forced by [&hellip;]","thumbnail_url":"https:\/\/engineering.jhu.edu\/zaki\/wp-content\/uploads\/2014\/10\/ThreePlanesNewMovieSnap.png"}