{"id":616,"date":"2024-05-31T16:05:00","date_gmt":"2024-05-31T20:05:00","guid":{"rendered":"https:\/\/carleton.ca\/aeroacoustics\/?p=616"},"modified":"2025-04-24T11:36:13","modified_gmt":"2025-04-24T15:36:13","slug":"zach-huffman-work-published-in-aerospace","status":"publish","type":"post","link":"https:\/\/carleton.ca\/aeroacoustics\/2024\/zach-huffman-work-published-in-aerospace\/","title":{"rendered":"Zach Huffman&#8217;s work published in the Aerospace Journal"},"content":{"rendered":"\n<section class=\"w-screen px-6 cu-section cu-section--white ml-offset-center md:px-8 lg:px-14\">\n    <div class=\"space-y-6 cu-max-w-child-5xl  md:space-y-10 cu-prose-first-last\">\n\n            <div class=\"cu-textmedia flex flex-col lg:flex-row mx-auto gap-6 md:gap-10 my-6 md:my-12 first:mt-0 max-w-5xl\">\n        <div class=\"justify-start cu-textmedia-content cu-prose-first-last\" style=\"flex: 0 0 100%;\">\n            <header class=\"font-light prose-xl cu-pageheader md:prose-2xl cu-component-updated cu-prose-first-last\">\n                                    <h1 class=\"cu-prose-first-last font-semibold !mt-2 mb-4 md:mb-6 relative after:absolute after:h-px after:bottom-0 after:bg-cu-red after:left-px text-3xl md:text-4xl lg:text-5xl lg:leading-[3.5rem] pb-5 after:w-10 text-cu-black-700 not-prose\">\n                        Zach Huffman&#8217;s work published in the Aerospace Journal\n                    <\/h1>\n                \n                                \n                            <\/header>\n\n                    <\/div>\n\n            <\/div>\n\n    <\/div>\n<\/section>\n\n<p>Congratulations to Zach for having published the journal article \u201cThe Derivation of an Empirical Model to Estimate the Power Spectral Density of Turbulent Boundary Layer Wall Pressure in Aircraft Using Machine Learning Regression Techniques\u201d in the Aerospace journal!<\/p>\n","protected":false},"excerpt":{"rendered":"<p>Congratulations to Zach for having published the journal article \u201cThe Derivation of an Empirical Model to Estimate the Power Spectral Density of Turbulent Boundary Layer Wall Pressure in Aircraft Using Machine Learning Regression Techniques\u201d in the Aerospace journal!<\/p>\n","protected":false},"author":2,"featured_media":0,"comment_status":"closed","ping_status":"closed","sticky":false,"template":"","format":"standard","meta":{"_acf_changed":false,"footnotes":"","_links_to":"","_links_to_target":""},"categories":[1],"tags":[],"class_list":["post-616","post","type-post","status-publish","format-standard","hentry","category-news"],"acf":{"cu_post_thumbnail":""},"_links":{"self":[{"href":"https:\/\/carleton.ca\/aeroacoustics\/wp-json\/wp\/v2\/posts\/616","targetHints":{"allow":["GET"]}}],"collection":[{"href":"https:\/\/carleton.ca\/aeroacoustics\/wp-json\/wp\/v2\/posts"}],"about":[{"href":"https:\/\/carleton.ca\/aeroacoustics\/wp-json\/wp\/v2\/types\/post"}],"author":[{"embeddable":true,"href":"https:\/\/carleton.ca\/aeroacoustics\/wp-json\/wp\/v2\/users\/2"}],"replies":[{"embeddable":true,"href":"https:\/\/carleton.ca\/aeroacoustics\/wp-json\/wp\/v2\/comments?post=616"}],"version-history":[{"count":1,"href":"https:\/\/carleton.ca\/aeroacoustics\/wp-json\/wp\/v2\/posts\/616\/revisions"}],"predecessor-version":[{"id":617,"href":"https:\/\/carleton.ca\/aeroacoustics\/wp-json\/wp\/v2\/posts\/616\/revisions\/617"}],"wp:attachment":[{"href":"https:\/\/carleton.ca\/aeroacoustics\/wp-json\/wp\/v2\/media?parent=616"}],"wp:term":[{"taxonomy":"category","embeddable":true,"href":"https:\/\/carleton.ca\/aeroacoustics\/wp-json\/wp\/v2\/categories?post=616"},{"taxonomy":"post_tag","embeddable":true,"href":"https:\/\/carleton.ca\/aeroacoustics\/wp-json\/wp\/v2\/tags?post=616"}],"curies":[{"name":"wp","href":"https:\/\/api.w.org\/{rel}","templated":true}]}}