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Micromechanical Models for Bending Behavior of Woven Composites
www-civ.eng.cam.ac.uk/dsl/publications/AIAA-2005-2264.pdf17 May 2005: 0. 100. 200. 300. 400. 500. 600. 0.00 0.20 0.40 0.60 0.80 1.00 1.20. ... 15. 20. 25. 0.00 0.03 0.06 0.09 0.12. Curvature (1/mm). Mo. -
AIAA 2004-1529Multi-Configuration Space FramesT. Schioler and S.…
www-civ.eng.cam.ac.uk/dsl/Schioler/publications/SDM2004.pdf30 Jan 2005: Figure 20 shows the measured force-displacement characteristics as well as the theoreticalresponse derived by assuming elastic axial shorteningand Euler buckling. ... 10. 15. Force. (N). Displacement (mm). Fig. 20 Comparison of theoretical and -
Design & Manufacture of Stiffened Spring-Back Reflector…
www-civ.eng.cam.ac.uk/dsl/publications/AIAA-2005-2048.pdf17 May 2005: Hence the curvedstiffener is a circular arc of r = 20 mm subtending anangle of 69. ... The first 20 eigenmodes wereextracted and the maximum frequency of interest wasset to 40 Hz. -
Thin-Shell Deployable Reflectors with Collapsible Stiffeners: Part I…
www-civ.eng.cam.ac.uk/dsl/publications/Reflectors-with-stiffeners.pdf1 Mar 2005: frequency ratios. Dividing Equation 20 by Equation 16 and simplifying, or alternatively taking directly. ... modes and, while Equation 20 may still be reasonably accurate in predicting the frequency.
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