NASA NTRS · 19680043268
Engineering estimates for supersonic flutter of curved shell segments.
Abstract
Cylindrical shell segments supersonic flutter boundaries engineering estimates related to Saturn 5 booster, obtaining thickness requirement as function of panel geometry
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Anderson, W. J., Hsu, K.-H.. 1968-04-01. Engineering estimates for supersonic flutter of curved shell segments.. https://ntrs.nasa.gov/citations/19680043268
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