Nonlinear Response of a Skin Panel under Combined Thermal and Structural Loading
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Miami University / OhioLINK
2012
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ndltd-OhioLink-oai-etd.ohiolink.edu-miami13447318182021-08-03T05:41:42Z Nonlinear Response of a Skin Panel under Combined Thermal and Structural Loading Ling, Yu Mechanical Engineering hypersonic aircraft skin panel nonlinear response thermal buckling snap-through <p>Future hypersonic vehicle will operate in an extreme environment, which involves extreme aerodynamic heating, fluctuating pressure and acoustic loading. Hypersonic vehicle must be reusable, lightweight and affordable in such environment. For hypersonic flight, the structure experiences complex aeroacoustic loads. The design of the structure depends on the ability to predict the response and the life of structure in extreme environment. This research presents adetailed investigation of the interactions and interplay among these parameters as evidenced by the nonlinear (static and dynamic) response of the panel.</p><p>A representative panel was selected as part of a ramp skin panel on a blend wing body hypersonic vehicle concept. This project focuses on the nonlinear response of the skin panel under combined thermal and structural loading. Thermal buckling, snap-through, and snap-buckling behaviors have been investigated by using different structural boundary condition. The long term goal of this research includes capturing fluid structure interaction as well asdeveloping design curves for nonlinear response of the panel.</p> 2012-08-15 English text Miami University / OhioLINK http://rave.ohiolink.edu/etdc/view?acc_num=miami1344731818 http://rave.ohiolink.edu/etdc/view?acc_num=miami1344731818 unrestricted This thesis or dissertation is protected by copyright: all rights reserved. It may not be copied or redistributed beyond the terms of applicable copyright laws. |
| collection |
NDLTD |
| language |
English |
| sources |
NDLTD |
| topic |
Mechanical Engineering hypersonic aircraft skin panel nonlinear response thermal buckling snap-through |
| spellingShingle |
Mechanical Engineering hypersonic aircraft skin panel nonlinear response thermal buckling snap-through Ling, Yu Nonlinear Response of a Skin Panel under Combined Thermal and Structural Loading |
| author |
Ling, Yu |
| author_facet |
Ling, Yu |
| author_sort |
Ling, Yu |
| title |
Nonlinear Response of a Skin Panel under Combined Thermal and Structural Loading |
| title_short |
Nonlinear Response of a Skin Panel under Combined Thermal and Structural Loading |
| title_full |
Nonlinear Response of a Skin Panel under Combined Thermal and Structural Loading |
| title_fullStr |
Nonlinear Response of a Skin Panel under Combined Thermal and Structural Loading |
| title_full_unstemmed |
Nonlinear Response of a Skin Panel under Combined Thermal and Structural Loading |
| title_sort |
nonlinear response of a skin panel under combined thermal and structural loading |
| publisher |
Miami University / OhioLINK |
| publishDate |
2012 |
| url |
http://rave.ohiolink.edu/etdc/view?acc_num=miami1344731818 |
| work_keys_str_mv |
AT lingyu nonlinearresponseofaskinpanelundercombinedthermalandstructuralloading |
| _version_ |
1719423724935970816 |