Analytical and experimental studies of natural vibration modes of ring-stiffened truncated-cone shells with variable theoretical ring fixity

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086 0 ‡aNAS 1.14:D-6473
088 ‡aNASA-TN-D-6473
100 1 ‡aNaumann, Eugene C.
245 1 0 ‡aAnalytical and experimental studies of natural vibration modes of ring-stiffened truncated-cone shells with variable theoretical ring fixity / ‡cEugene C. Naumann, Donnell S. Catherines, and William C. Walton, Jr.
246 3 ‡aNASA TN D-6473
260 ‡aWashington, D.C. : ‡bNational Aeronautics and Space Administration ; ‡a[For sale by the Clearinghouse for Federal Scientific and Technical, Springfield, Virginia 22151], ‡c1971.
300 ‡a84 p. : ‡bill. ; ‡c27 cm.
490 0 ‡aNASA technical note ; ‡vD-6473
504 ‡aIncludes bibliographical references (p. 34).
520 ‡aExperimental and analytical investigations of the vibratory behavior of ring-stiffened truncated-cone shells are described. Vibration tests were conducted on (1) 60 [degree] conical shells having up to four ring stiffeners and for free-free and clamped-free edge constraints and (2) 90 [degree] conical shells, for two thicknesses, each with two angle rings and for free-free, free-clamped, and clamped-clamped edge constraints. The analytical method is based on linear thin-shell theory, employing the Rayleigh-Ritz method. Discrete rings are represented as composed of one or more segments, each of which is a short truncated-cone shell of uniform thickness. Equations of constraint are used to join a ring and shell along a circumferential line connection. Excellent agreement was obtained for comparisons of experimental and calculated frequencies.
538 ‡aMode of access: Internet.
650 0 ‡aConical shells ‡xVibration.
650 0 ‡aShells (Engineering) ‡xVibration.
700 1 ‡aWalton, William C.
700 1 ‡aCatherines, Donnell S.
710 2 ‡aLangley Research Center.
710 1 ‡aUnited States. ‡bNational Aeronautics and Space Administration.
CID ‡a011443402
DAT 0 ‡a20101110111407.0 ‡b20141009010000.0
DAT 1 ‡a20141112165512.0 ‡b2023-03-14T18:25:53Z
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