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Deployable Tensegrity Structures for Space Applications
www-civ.eng.cam.ac.uk/dsl/publications/TibertDocThesis.pdf30 Jul 2002: l2c = 2R2(1 cos θ) H2, (3.2a). l2s = 2R2. [1 cos. ( ... Φ Matrix of bar flexibilities (b b), p. 59ω Element stress (equivalent to q), p.
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