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  • About
  • The Global ETD Search service is a free service for researchers to find electronic theses and dissertations. This service is provided by the Networked Digital Library of Theses and Dissertations.
    Our metadata is collected from universities around the world. If you manage a university/consortium/country archive and want to be added, details can be found on the NDLTD website.
71

Three-dimensional modeling of rigid pavement

Beegle, David J. January 1998 (has links)
Thesis (M.S.)--Ohio University, August, 1998. / Title from PDF t.p.
72

Large 3-D deflection and force analysis of lateral torsional buckled beams /

Chase, Robert P. January 2006 (has links) (PDF)
Thesis (M.S.)--Brigham Young University. Dept. of Mechanical Engineering, 2006. / Includes bibliographical references (p. 81-82).
73

Behavior of three-span braced columns with equal and unequal spans /

Yang, Yu-Wen, January 1993 (has links)
Thesis (M.S.)--Virginia Polytechnic Institute and State University, 1993. / Vita. Abstract. Includes bibliographical references (leaves 125-126). Also available via the Internet.
74

Testing and assessment of FRP strengthened concrete T-beam bridges in Pennsylvania

Justice, Adam L. January 2010 (has links)
Thesis (M.S.)--West Virginia University, 2010. / Title from document title page. Document formatted into pages; contains ix, 223 p. : ill. (some col.). Includes abstract. Includes bibliographical references (p. 138-141).
75

Mechanotransduction in engineered cartilaginous tissues in vitro oscillatory tensile loading /

Vanderploeg, Eric James. January 2006 (has links)
Thesis (Ph. D.)--Mechanical Engineering, Georgia Institute of Technology, 2007. / Radhakrishna, Harish, Committee Member ; LaPlaca, Michelle, Committee Member ; Nerem, Robert, Committee Member ; Garcia, Andres, Committee Member ; Levenston, Marc, Committee Chair.
76

Full scale static lateral load test of a 9 pile group in sand /

Christensen, Dustin Shaun, January 2006 (has links) (PDF)
Thesis (M.S.)--Brigham Young University. Dept. of Civil and Environmental Engineering, 2006. / Includes bibliographical references (p. 163-166).
77

Effects of axial load, shielding and shape on negative skin friction on piles /

Lam, Sze Yue. January 2006 (has links)
Thesis (M.Phil.)--Hong Kong University of Science and Technology, 2006. / Includes bibliographical references (leaves 263-272). Also available in electronic version.
78

Load ratings using an in-service bridge monitoring system

Brookes, Briana O. January 2007 (has links)
Thesis (M.C.E.)--University of Delaware, 2007. / Principal faculty advisors: Harry Shenton and Michael J. Chajes, Dept. of Civil & Environmental Engineering. Includes bibliographical references.
79

Gust response and its alleviation for a hingeless helicopter rotor in cruising flight.

Yasue, Masahiro January 1977 (has links)
Thesis. 1977. Ph.D.--Massachusetts Institute of Technology. Dept. of Aeronautics and Astronautics. / MICROFICHE COPY AVAILABLE IN ARCHIVES AND AERONAUTICS. / Vita. / Includes bibliographical references. / Ph.D.
80

Structural Analysis and Testing of a Carbon-Composite Wing using Fiber Bragg Gratings

Nicolas, Matthew James 11 May 2013 (has links)
The objective of this study was to determine the deflected wing shape and the out-of-plane loads of a large-scale carbon-composite wing of an ultralight aerial vehicle using Fiber Bragg Grating (FBG) technology. The composite wing was instrumented with an optical fiber on its top and bottom surfaces positioned over the main spar, resulting in approximately 780 strain sensors bonded to the wings. The strain data from the FBGs was compared to that obtained from four conventional strain gages, and was used to obtain the out-of-plane loads as well as the wing shape at various load levels using NASA-developed real-time load and displacement algorithms. The composite wing measured 5.5 meters and was fabricated from laminated carbon uniaxial and biaxial prepreg fabric with varying laminate ply patterns and wall thickness dimensions. A three-tier whiffletree system was used to load the wing in a manner consistent with an inlight loading condition.

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