Loosely coupled, modular framework for linear static aeroelastic analyses
A computational framework for linear static aeroelastic analyses is presented. The overall aeroelasticity model is applicable to conceptual aircraft design studies and other low-fidelity aero-structural analyses. A partitioned approach is used, i. e. separate solvers for aerodynamics and structure a...
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| Format: | Others |
| Language: | English |
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KTH, Lättkonstruktioner
2019
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| Online Access: | http://urn.kb.se/resolve?urn=urn:nbn:se:kth:diva-262047 |