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1	Determination of the dynamic characteristics of a ten-storey steel building. Leung, Mang-chiu. January 1971 (has links) Thesis--M. Sc.(Eng.), University of Hong Kong. / Mimeographed.
2	A distribution procedure for the dynamic analysis of multistorey building frames / Chu, Sau-kong. January 1967 (has links) Thesis (M. Sc. (Eng.))--University of Hong kong. / Mimeographed.
3	State space modeling and identification of stochastic linear structural systems Pridham, Brad A. Wilson, John C. January 2004 (has links) Thesis (Ph.D.)--McMaster University, 2005. / Supervisor: John C. Wilson. Includes bibliographical references (leaves 299-310).
4	Semi-active management of blast load structural response : a thesis submitted in partial fulfilment of the requirements for the degree of Master of Mechanical Engineering in the University of Canterbury / Ewing, C. M. January 2007 (has links) Thesis (M.E.)--University of Canterbury, 2007. / Typescript (photocopy). Includes bibliographical references (leaves 105-106). Also available via the World Wide Web.
5	A computational framework for dynamic soil-structure interaction analysis / Sribalaskandarajah, Kandiah. January 1996 (has links) Thesis (Ph. D.)--University of Washington, 1996. / Vita. Includes bibliographical references (leaves 114-122).
6	An efficient eigensolution method and its implementation for large structural systems Kim, Mintae, Bennighof, Jeffrey Kent, January 2004 (has links) (PDF) Thesis (Ph. D.)--University of Texas at Austin, 2004. / Supervisor: Jeffrey K. Bennighof. Vita. Includes bibliographical references.
7	Dynamic Analysis of Plane Frames Malekamdani, Zohreh 01 January 1983 (has links) No description available.
8	Implementation of automated multilevel substructuring for frequency response analysis of structures Kaplan, Matthew Frederick. January 2001 (has links) Thesis (Ph. D.)--University of Texas at Austin, 2001. / Vita. Includes bibliographical references. Available also from UMI/Dissertation Abstracts International.
9	Relating constrained motion to force through Newton's second law Roithmayr, Carlos. January 2007 (has links) Thesis (Ph. D.)--Aerospace Engineering, Georgia Institute of Technology, 2007. / Bauchau, Olivier, Committee Member ; Hodges, Dewey, Committee Chair ; Singhose, William, Committee Member ; Costello, Mark, Committee Member ; Flannery, Raymond, Committee Member.
10	Development And Comparative Evaluation Of A New Structural Modification Method In Application To Aircraft Structures Koksal, Sertac 01 September 2006 (has links) (PDF) In the development of engineering products, it is necessary to predict dynamic properties of the modified structures. Achieving such predictions by using the structural properties of the original structure and information on the modifications is commonly referred to as structural modification analysis. In this thesis, &Ouml / zg&uuml / ven&rsquo / s Structural Modification Method and Sherman-Morrison Method are selected as exact methods for structural modifications to predict the dynamics of a locally modified structure. Also, a new structural modification method named as &ldquo / Extended Successive Matrix Inversion Method&rdquo / is developed in this study. These three methods are implemented in a software developed herein, called &ldquo / Structural Modification Toolbox&rdquo / . The software uses modal analysis results of MSC Nastran&copy / for the original structure and calculates the modified frequency response functions by any of the methods above. In order to validate the software, direct modal analysis results of MSC Nastran&copy / for the frequency response functions of the modified structure are used. The methods are compared in terms of computational time, and the effectivity of each method is studied as a function of modification size to determine which of these methods is more suitable. In order to investigate the application of the methods and compare their results with experimental ones, modal tests are conducted on a scaled aircraft structure. The solutions are compared with test results obtained from modified test structure. Additionally, the software is used for comparison of real aircraft test results and frequency response functions of the modified structure.

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