Fuzzy programming approach to UAV preliminary sizing

In preliminary sizing, wing loading, power loading, and maximum lift coefficient are commonly determined through an informal optimization process using statistical equations based on existing aircraft data in conjunction with a matching chart from which the best design point is picked. Presented her...

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Bibliographic Details
Main Authors: Banal, Lemuel F., Ubando, Aristotle T.
Format: text
Published: Animo Repository 2016
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Online Access:https://animorepository.dlsu.edu.ph/faculty_research/1538
https://animorepository.dlsu.edu.ph/context/faculty_research/article/2537/type/native/viewcontent
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Institution: De La Salle University

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