<?xml version="1.0" encoding="UTF-8"?><ns2:project xmlns:ns1="http://gtr.rcuk.ac.uk/gtr/api" xmlns:ns2="http://gtr.rcuk.ac.uk/gtr/api/project" xmlns:ns3="http://gtr.rcuk.ac.uk/gtr/api/fund" xmlns:ns4="http://gtr.rcuk.ac.uk/gtr/api/person" xmlns:ns5="http://gtr.rcuk.ac.uk/gtr/api/project/outcome" xmlns:ns6="http://gtr.rcuk.ac.uk/gtr/api/organisation" ns1:created="2026-06-03T15:52:43Z" ns1:href="http://gtr.ukri.org/gtr/api/projects/EB3568D0-12D9-4102-83DA-FD5804E82A8E" ns1:id="EB3568D0-12D9-4102-83DA-FD5804E82A8E"><ns1:links><ns1:link ns1:href="http://gtr.ukri.org/gtr/api/persons/CC649258-0AF1-49D4-8955-72A750EA58F1" ns1:rel="PM_PER"/><ns1:link ns1:href="http://gtr.ukri.org/gtr/api/organisations/A1899136-AC06-4A29-9DB5-6E18B8077BEE" ns1:rel="LEAD_ORG"/><ns1:link ns1:href="http://gtr.ukri.org/gtr/api/organisations/6B57D64D-182B-4847-8A8F-366E0669D013" ns1:rel="PARTICIPANT_ORG"/><ns1:link ns1:href="http://gtr.ukri.org/gtr/api/organisations/A1899136-AC06-4A29-9DB5-6E18B8077BEE" ns1:rel="PARTICIPANT_ORG"/><ns1:link ns1:href="http://gtr.ukri.org/gtr/api/organisations/57FBB945-1548-437A-84C2-D8D4385901B5" ns1:rel="PARTICIPANT_ORG"/><ns1:link ns1:end="2018-04-29T23:00:00Z" ns1:href="http://gtr.ukri.org/gtr/api/funds/FB2D28CA-69D1-4638-AF9A-9C5BECA3F9C8" ns1:rel="FUND" ns1:start="2015-11-01T00:00:00Z"/></ns1:links><ns2:identifiers><ns2:identifier ns2:type="RCUK">102369</ns2:identifier></ns2:identifiers><ns2:title>Heatssim: Holistic Engineering Approach to Thermal and Structural Simulation</ns2:title><ns2:status>Closed</ns2:status><ns2:grantCategory>Collaborative R&amp;D</ns2:grantCategory><ns2:leadFunder>Innovate UK</ns2:leadFunder><ns2:abstractText>The Heatssim (Holistic Engineering Approach to Thermal and Structural Simulation) project aims to deliver an optimised design process for aerospace gearboxes, providing a step-change in the design and analysis methods for the development of state-of-the-art and future aerospace transmission systems. This is achieved by a multi-disciplinary and multi-physics analysis of an aerospace gearbox, allowing investigation of the interaction between CFD, thermal, static deflections, fatigue and dynamic phenomena. A multi-fidelity analysis procedure will be established, identifying the optimum level of fidelity required to achieve the necessary accuracy for each phenomenon, resulting in a repeatable simulation process and maximum analysis speed. The process will be productised via a reputable CAE environment which is currently used by leading aerospace companies.</ns2:abstractText></ns2:project>