<?xml version="1.0" encoding="UTF-8"?><rss version="2.0" xmlns:dc="http://purl.org/dc/elements/1.1/"><channel><title>CR4 - Section&#x3a; Aerospace</title><link>https&#x3a;&#x2f;&#x2f;cr4.globalspec.com&#x2f;section&#x2f;aerospace</link><description><![CDATA[The Aerospace Section of CR4 includes forum and blog entries about aircraft, spacecraft, and all of the &#x22;space&#x22; surrounding them.]]></description><copyright>Copyright 2026</copyright><pubDate>Sat, 04 Jul 2026 03:05:51 EST</pubDate><generator>https&#x3a;&#x2f;&#x2f;cr4.globalspec.com</generator><item><title><![CDATA[Equivalent Stress in Structure During Resonance&#x3f;]]></title><link><![CDATA[https&#x3a;&#x2f;&#x2f;cr4.globalspec.com&#x2f;thread&#x2f;151583&#x2f;Equivalent-Stress-in-Structure-During-Resonance&#x3f;from_rss&#x3d;1]]></link><description><![CDATA[Is it possible to estimate or to get input for stress calculation for instance in exhaust system during it&#x27;s resonance behaviour. Then you have to create calculation of structural deformation in this frequency point. I have developed calculation method based on OVA measurement when in certain orders]]></description><pubDate>Sat, 04 Jul 2026 03&#x3a;05&#x3a;51 EST</pubDate><guid><![CDATA[https&#x3a;&#x2f;&#x2f;cr4.globalspec.com&#x2f;thread&#x2f;151583&#x2f;Equivalent-Stress-in-Structure-During-Resonance]]></guid><dc:creator>Reino Eskelinen</dc:creator><dc:subject>Aerospace</dc:subject></item></channel></rss>