DESIGN OF AN AIRCRAFT MAIN WING SPARExplore further
2018-11-16u2002·u2002The design of this wing spar is limited to specific design constraints. These constraints are displayed below in Table 3. Table 3 - Design Constraints ( A E E 471 P r oj e c t 2 Handout - Dav i ds on) Height (h) in Depth (b) in Thickness in tw/tf in 4≤h ≤8 3≤b ≤6 Flange or …
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