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Researchers extend the boundaries for integration and application of multidisciplinary design optimization
Researchers extend the boundaries for integration and application of multidisciplinary design optimization. From January through July, researchers at the University of Michigan developed an aeropropulsive high-bypass turbofan model that integrates one-dimensional thermodynamic cycle modeling and com...
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Published in: | Aerospace America 2022-12, Vol.60 (11) |
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creator | Henson, Mike Hardin, Chris Cataldo, Giuseppe |
description | Researchers extend the boundaries for integration and application of multidisciplinary design optimization. From January through July, researchers at the University of Michigan developed an aeropropulsive high-bypass turbofan model that integrates one-dimensional thermodynamic cycle modeling and computational fluid dynamics within Mphys, a multiphysics library built on top of the OpenMDAO computer program created by NASA's Glenn Research Center in Ohio. In June, a team of NASA and Caltech researchers finalized a rank statistics-based multifidelity global sensitivity analysis, or GSA, method that does not depend on the number of model parameters. In July, Airbus and the University of Michigan concluded a five-year research effort that created novel methods for optimizing very flexible, high-aspect-ratio wings. |
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From January through July, researchers at the University of Michigan developed an aeropropulsive high-bypass turbofan model that integrates one-dimensional thermodynamic cycle modeling and computational fluid dynamics within Mphys, a multiphysics library built on top of the OpenMDAO computer program created by NASA's Glenn Research Center in Ohio. In June, a team of NASA and Caltech researchers finalized a rank statistics-based multifidelity global sensitivity analysis, or GSA, method that does not depend on the number of model parameters. 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From January through July, researchers at the University of Michigan developed an aeropropulsive high-bypass turbofan model that integrates one-dimensional thermodynamic cycle modeling and computational fluid dynamics within Mphys, a multiphysics library built on top of the OpenMDAO computer program created by NASA's Glenn Research Center in Ohio. In June, a team of NASA and Caltech researchers finalized a rank statistics-based multifidelity global sensitivity analysis, or GSA, method that does not depend on the number of model parameters. In July, Airbus and the University of Michigan concluded a five-year research effort that created novel methods for optimizing very flexible, high-aspect-ratio wings.</description><subject>Aeronautical research</subject><subject>Aerospace engineering</subject><subject>Boundaries</subject><subject>Computational fluid dynamics</subject><subject>Design optimization</subject><subject>High aspect ratio</subject><subject>Multidisciplinary design optimization</subject><subject>Research facilities</subject><subject>Sensitivity analysis</subject><subject>Turbofans</subject><issn>0740-722X</issn><fulltext>true</fulltext><rsrctype>article</rsrctype><creationdate>2022</creationdate><recordtype>article</recordtype><sourceid/><recordid>eNotjU9LxDAUxHNQcF39DgHPhdemzUuPsvgPFoRFwduSNi-7Kd2kJimon97iehpm5sfMBVsB1lBgVX1cseuUBgBohGhXbNhRIh37I8XE6SuTNzwfiXdh9kZHR4nbELnzmQ5RZxc81wuip2l0_dkHy0_zmJ1xqXdL7HX85oaSOyzdlN3J_fyBN-zS6jHR7b-u2fvjw9vmudi-Pr1s7rfFVJYiF7IsuxaQLArQiNj2WhOqBhvbgelMVSqLUkgCKSyC0NCWvZRYk2gQlBBrdnfenWL4nCnl_RDm6JfLfYW1UgraVolfDLNU9g</recordid><startdate>20221201</startdate><enddate>20221201</enddate><creator>Henson, Mike</creator><creator>Hardin, Chris</creator><creator>Cataldo, Giuseppe</creator><general>American Institute of Aeronautics and Astronautics</general><scope/></search><sort><creationdate>20221201</creationdate><title>Researchers extend the boundaries for integration and application of multidisciplinary design optimization</title><author>Henson, Mike ; Hardin, Chris ; Cataldo, Giuseppe</author></sort><facets><frbrtype>5</frbrtype><frbrgroupid>cdi_FETCH-LOGICAL-p113t-611b907ef730a7779caae78575fb0dbd218f7636e063f703a091c6674e3570833</frbrgroupid><rsrctype>articles</rsrctype><prefilter>articles</prefilter><language>eng</language><creationdate>2022</creationdate><topic>Aeronautical research</topic><topic>Aerospace engineering</topic><topic>Boundaries</topic><topic>Computational fluid dynamics</topic><topic>Design optimization</topic><topic>High aspect ratio</topic><topic>Multidisciplinary design optimization</topic><topic>Research facilities</topic><topic>Sensitivity analysis</topic><topic>Turbofans</topic><toplevel>peer_reviewed</toplevel><toplevel>online_resources</toplevel><creatorcontrib>Henson, Mike</creatorcontrib><creatorcontrib>Hardin, Chris</creatorcontrib><creatorcontrib>Cataldo, Giuseppe</creatorcontrib><jtitle>Aerospace America</jtitle></facets><delivery><delcategory>Remote Search Resource</delcategory><fulltext>fulltext</fulltext></delivery><addata><au>Henson, Mike</au><au>Hardin, Chris</au><au>Cataldo, Giuseppe</au><format>journal</format><genre>article</genre><ristype>JOUR</ristype><atitle>Researchers extend the boundaries for integration and application of multidisciplinary design optimization</atitle><jtitle>Aerospace America</jtitle><date>2022-12-01</date><risdate>2022</risdate><volume>60</volume><issue>11</issue><issn>0740-722X</issn><abstract>Researchers extend the boundaries for integration and application of multidisciplinary design optimization. From January through July, researchers at the University of Michigan developed an aeropropulsive high-bypass turbofan model that integrates one-dimensional thermodynamic cycle modeling and computational fluid dynamics within Mphys, a multiphysics library built on top of the OpenMDAO computer program created by NASA's Glenn Research Center in Ohio. In June, a team of NASA and Caltech researchers finalized a rank statistics-based multifidelity global sensitivity analysis, or GSA, method that does not depend on the number of model parameters. In July, Airbus and the University of Michigan concluded a five-year research effort that created novel methods for optimizing very flexible, high-aspect-ratio wings.</abstract><cop>New York</cop><pub>American Institute of Aeronautics and Astronautics</pub></addata></record> |
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subjects | Aeronautical research Aerospace engineering Boundaries Computational fluid dynamics Design optimization High aspect ratio Multidisciplinary design optimization Research facilities Sensitivity analysis Turbofans |
title | Researchers extend the boundaries for integration and application of multidisciplinary design optimization |
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