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20141009010000.0 |
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050125s1971 dcua b f000 0 eng d |
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‡asdr-uiuc6403354
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‡a(OCoLC)642477474
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‡aEGM
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‡aUIUU
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‡aNAS 1.14:D-6473
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‡aNASA-TN-D-6473
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‡aNaumann, Eugene C.
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‡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.
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‡aNASA TN D-6473
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‡aWashington, D.C. :
‡bNational Aeronautics and Space Administration ;
‡a[For sale by the Clearinghouse for Federal Scientific and Technical, Springfield, Virginia 22151],
‡c1971.
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‡a84 p. :
‡bill. ;
‡c27 cm.
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‡aNASA technical note ;
‡vD-6473
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‡aIncludes bibliographical references (p. 34).
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‡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.
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‡aMode of access: Internet.
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‡aConical shells
‡xVibration.
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‡aShells (Engineering)
‡xVibration.
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‡aWalton, William C.
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‡aCatherines, Donnell S.
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‡aLangley Research Center.
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‡aUnited States.
‡bNational Aeronautics and Space Administration.
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‡a20101110111407.0
‡b20141009010000.0
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‡a20141112165512.0
‡b2023-03-14T18:25:53Z
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‡lloader.pl-003-020
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‡bUIU
‡cUIUC
‡d20230314
‡sgoogle
‡uuiug.30112106692186
‡y1971
‡rpd
‡qbib
‡tUS fed doc
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