Analysis of shells of revolution under axisymmetrical loading using the quadrature method

Analysis of shells of revolution under axisymmetrical loading using the quadrature method

To complete study [1], the procedure of applying the numerical quadrature method to analyzing the shells of revolution under axisymmetrical loading is presented.

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Bibliographische Detailangaben
Veröffentlicht in:Russian aeronautics 2010-06, Vol.53 (2), p.230-234
1. Verfasser: Akhmed’yanov, I. S.
Format: Artikel
Sprache:eng
Schlagworte:
Automotive Engineering
Engineering
Mathematical models
Quadratures
Shells of revolution
Technical Notes Structural Mechanics and Strength of Flight Vehicles
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Beschreibung
Zusammenfassung:To complete study [1], the procedure of applying the numerical quadrature method to analyzing the shells of revolution under axisymmetrical loading is presented.
ISSN:1068-7998
1934-7901
DOI:10.3103/S1068799810020182