Methods for the Aerostructural Design and Optimization of Wings with Arbitrary Planform and Payload Distribution
The design of an aircraft wing often involves the use of mathematical methods for simultaneous aerodynamic and structural design. The goal of many of these methods is to minimize the drag on the wing. A variety of computer models exist for this purpose, but some require the use of expensive time and...
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| Format: | Others |
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DigitalCommons@USU
2018
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| Online Access: | https://digitalcommons.usu.edu/etd/6909 https://digitalcommons.usu.edu/cgi/viewcontent.cgi?article=8012&context=etd |