{"id":30674,"date":"2025-01-23T01:26:31","date_gmt":"2025-01-23T01:26:31","guid":{"rendered":"https:\/\/stateaviationjournal.com\/?p=30674"},"modified":"2025-01-23T01:27:24","modified_gmt":"2025-01-23T01:27:24","slug":"design-analysis-software-enables-swift-engineering-to-optimize-35ft-nose-cone-structure-of-x-59-aircraft-designed-for-quieting-sonic-booms","status":"publish","type":"post","link":"https:\/\/stateaviationjournal.com\/index.php\/national-news\/design-analysis-software-enables-swift-engineering-to-optimize-35ft-nose-cone-structure-of-x-59-aircraft-designed-for-quieting-sonic-booms\/%20","title":{"rendered":"Design &amp; Analysis Software Enables Swift Engineering to Optimize 35ft Nose Cone Structure of X-59 Aircraft &#8211; Designed for Quieting Sonic Booms"},"content":{"rendered":"\n<p class=\"\"><em>Photo above &#8211; The X-59, a unique experimental aircraft from Lockheed Martin Skunk Works\u00ae, is part of the Quesst (Quiet Supersonic Technology) mission of U.S. National Aeronautics and Space Administration (NASA) to quiet loud sonic booms. Photo Credits: Lockheed Martin \/ NASA.<\/em><\/p>\n\n\n\n<p class=\"\"><a href=\"https:\/\/collieraerospace.com\/\" data-type=\"link\" data-id=\"https:\/\/collieraerospace.com\/\">Collier Aerospace Corp<\/a>., developer of the HyperX\u00ae computer-aided engineering (CAE) solution, has announced that its design and analysis software was chosen by Swift Engineering, Inc., for structural sizing, analysis and test validation of the low-boom X-59 aircraft\u2019s nose cone. This experimental aircraft from Lockheed Martin Skunk Works\u00ae is part of the Quesst (Quiet Supersonic Technology) mission of U.S. National Aeronautics and Space Administration (NASA) to quiet loud sonic booms. Swift Engineering was contracted to build and perform structural analysis and certification testing for the X-59\u2019s distinctive, 35 ft.-long nose cone, designed to control aerodynamic pressure waves (shock waves), that form at the sharp nose tip during supersonic flight, resulting in quieter sonic booms.&nbsp;<\/p>\n\n\n<div class=\"wp-block-image\">\n<figure class=\"alignright size-full is-resized\"><img loading=\"lazy\" decoding=\"async\" width=\"622\" height=\"415\" src=\"https:\/\/stateaviationjournal.com\/wp-content\/uploads\/Collier-Aerospace-X-59.jpg\" alt=\"\" class=\"wp-image-30676\" style=\"width:370px;height:auto\" srcset=\"https:\/\/stateaviationjournal.com\/wp-content\/uploads\/Collier-Aerospace-X-59.jpg 622w, https:\/\/stateaviationjournal.com\/wp-content\/uploads\/Collier-Aerospace-X-59-300x200.jpg 300w\" sizes=\"auto, (max-width: 622px) 100vw, 622px\" \/><figcaption class=\"wp-element-caption\"><em>Collier Aerospace\u2019s design and analysis software was chosen by Swift Engineering, Inc., for structural sizing, analysis and test validation of the X-59 aircraft\u2019s nose cone. Photo Credits: Lockheed Martin \/ NASA.<\/em><\/figcaption><\/figure><\/div>\n\n\n<p class=\"\">Collier Aerospace\u2019s software enabled Swift Engineering to remove mass that reduced the nose cone\u2019s weight by over 25 percent while maintaining dimensional stability; evaluate the design for a wide range of load cases; and provide detailed stress reporting to support part release and fabrication. The company also used the software to perform detailed analyses, supporting structural testing substantiation of the structural design.&nbsp;<\/p>\n\n\n\n<p class=\"\">\u201cThe Collier Aerospace software played a critical role throughout this high-visibility project to design, engineer and build the X-59 nose structure,\u201d said Bill Giannetti, technical consultant to Swift Engineering. \u201cAt the outset, when the team from Skunk Works explained how important lightweighting was, I had so much confidence in the software that I was convinced we would remove 100 pounds from the nose cone. However, we surpassed that goal by achieving a significant weight savings of over 25 percent on the nose cone structure.\u201d<\/p>\n\n\n\n<p class=\"\">Giannetti added, \u201cWe were able to iterate the structural sizing software with our finite element analysis solver, which enabled weight reduction through structural optimization and rapid load path convergence. Once the system was set up, we could literally watch the mass come out of the nose structure, while meeting all the traditional aerospace failure criteria simultaneously. It\u2019s a fantastic software tool.\u201d<\/p>\n\n\n\n<p class=\"\"><strong>Meeting Rigorous Requirements<\/strong><\/p>\n\n\n\n<p class=\"\">To lower the weight of the approximately 400-lb. preliminary design, which specified graphite\/epoxy composite and a honeycomb-core sandwich structure, Swift Engineering\u2019s team removed unnecessary plies, simultaneously optimizing the structure for stress and stability. The Collier Aerospace software enabled the team to quickly evaluate design alternatives by considering trade-offs in ply-layup schedules and core panel and edge band thicknesses, and then rapidly evaluate the change to the section stiffness and deflection.<\/p>\n\n\n\n<p class=\"\">Swift Engineering used the full capabilities of the Collier Aerospace software for this unique aircraft nose structure, extending beyond preliminary sizing and optimization to include conducting detailed laminate strength analysis using design allowables derived from testing. The software enabled the company to deliver the nose cone ahead of schedule and under budget.<\/p>\n\n\n\n<p class=\"\">HyperX\u00ae software automates stress analysis and design. It performs rapid structural sizing to all load cases, lightweighting and margin writing. The software helps ensure the producibility of a composite part by creating a design that is optimized for manufacturability. It reduces schedule time by speeding up the engineering cycle and shortening the U.S. Federal Aviation Administration (FAA) and European Union Aviation Safety Agency (EASA) certification processes.<\/p>\n\n\n\n<p class=\"\"><strong>From Boom to \u201cThump\u201d<\/strong><\/p>\n\n\n\n<p class=\"\">The goal of the X-59 aircraft, which is expected to make its first flight in 2025, is to help establish an acceptable noise standard for commercial supersonic flights over land, potentially resulting in U.S. and international regulators lifting a five-decade-long ban that was imposed due to loud sonic booms. Thanks to its unique geometry, particularly the elongated nose cone, the X-59 is expected to generate a barely audible thump rather than a boom, reducing noise impacts.<\/p>\n\n\n\n<p class=\"\">\u201cWe\u2019re grateful that our software helped Swift Engineering achieve success with the X-59 nose cone and met the high expectations of Lockheed Martin Skunk Works,\u201d commented James Ainsworth, vice president, Engineering Services, Collier Aerospace. \u201cThe high level of credibility that our solution has earned, and its powerful sizing and analytical capabilities, were key factors in Swift\u2019s decision to choose our software. We\u2019re looking forward to the X-59\u2019s first flight.\u201d<\/p>\n","protected":false},"excerpt":{"rendered":"<p>Photo above &#8211; The X-59, a unique experimental aircraft from Lockheed Martin Skunk Works\u00ae, is part of the Quesst (Quiet Supersonic Technology) mission of U.S. National Aeronautics and Space Administration (NASA) to quiet loud sonic booms. Photo Credits: Lockheed Martin \/ NASA. Collier Aerospace Corp., developer of the HyperX\u00ae computer-aided engineering (CAE) solution, has announced [&hellip;]<\/p>\n","protected":false},"author":3,"featured_media":30675,"comment_status":"closed","ping_status":"open","sticky":false,"template":"","format":"standard","meta":{"_jetpack_memberships_contains_paid_content":false,"footnotes":""},"categories":[115],"tags":[],"class_list":["post-30674","post","type-post","status-publish","format-standard","has-post-thumbnail","hentry","category-national-news"],"jetpack_featured_media_url":"https:\/\/stateaviationjournal.com\/wp-content\/uploads\/X-59-.jpg","jetpack_sharing_enabled":true,"_links":{"self":[{"href":"https:\/\/stateaviationjournal.com\/index.php\/wp-json\/wp\/v2\/posts\/30674","targetHints":{"allow":["GET"]}}],"collection":[{"href":"https:\/\/stateaviationjournal.com\/index.php\/wp-json\/wp\/v2\/posts"}],"about":[{"href":"https:\/\/stateaviationjournal.com\/index.php\/wp-json\/wp\/v2\/types\/post"}],"author":[{"embeddable":true,"href":"https:\/\/stateaviationjournal.com\/index.php\/wp-json\/wp\/v2\/users\/3"}],"replies":[{"embeddable":true,"href":"https:\/\/stateaviationjournal.com\/index.php\/wp-json\/wp\/v2\/comments?post=30674"}],"version-history":[{"count":2,"href":"https:\/\/stateaviationjournal.com\/index.php\/wp-json\/wp\/v2\/posts\/30674\/revisions"}],"predecessor-version":[{"id":30678,"href":"https:\/\/stateaviationjournal.com\/index.php\/wp-json\/wp\/v2\/posts\/30674\/revisions\/30678"}],"wp:featuredmedia":[{"embeddable":true,"href":"https:\/\/stateaviationjournal.com\/index.php\/wp-json\/wp\/v2\/media\/30675"}],"wp:attachment":[{"href":"https:\/\/stateaviationjournal.com\/index.php\/wp-json\/wp\/v2\/media?parent=30674"}],"wp:term":[{"taxonomy":"category","embeddable":true,"href":"https:\/\/stateaviationjournal.com\/index.php\/wp-json\/wp\/v2\/categories?post=30674"},{"taxonomy":"post_tag","embeddable":true,"href":"https:\/\/stateaviationjournal.com\/index.php\/wp-json\/wp\/v2\/tags?post=30674"}],"curies":[{"name":"wp","href":"https:\/\/api.w.org\/{rel}","templated":true}]}}