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27 Aug 2002: 20 16 4.130 24 5.340 33 5.9. 6. Table 3: Tested configurations. ... Configuration Cuts Slits α β γ w(deg) (deg) (deg) (mm). O - - - - - -A 2 2 - 4 50 20B - 4 8 24 90 20.

14 Feb 2003: Mode 22 (41.81 Hz) Mode 23 (41.98 Hz) Mode 24 (44.32 Hz).

30 Jul 2002: Calladine studies a physical model of a tensegritystructure with 12 joints and 24 bars, which should be loose with 6 degrees of freedom,according to Maxwell’s rule; yet, it is

21 Mar 2001: 2.24). wherefromYoung(1989p.68). I x. =. R3t. 1. 3t 2R+. t2 R2. ... The transformation of the nodal coordinates is2. 4XYZ. 35 =. 24 cos sin 0sin cos 0.

12 Nov 2003: 24. 3.13 Example of two Non-holonomic Restrictions Being Violated and its Handling. ... Time. 41. 3.24 Force of Static Friction vs. Normal Force. 41.

14 Feb 2003: weobtain. T1TĀT3TB̄T1TC̄T3TD̄. (T1UĀT3TB̄T1TC̄T3TD̄) θ′A+(T1TĀT3UB̄T1TC̄T3TD̄) θ′B+(T1TĀT3TB̄T1UC̄T3TD̄) θ′C+(T1TĀT3TB̄T1TC̄T3UD̄) θ′D = I (24). From Equation 23, the first term in Equation 24 isequal to I E.

20 Jul 2007: α25 and β1, β2,. β25.However, only 24 design variables are needed to represent each grid design, due to symmetry anddue to a more advanced parameter smoothing process. ... Loading 1 kPa pressure loadingNumber of regions 25Number of design variables

27 Aug 2002: Offset 6 45.9Configuration 12 12.5(A = 1 m) 24 3.3. Table 1: Typical surface errors of reflectors with D = 10 m and F = 7.8 m.

14 Mar 2003: e11 =h1A2 h2A1. (h1h3 h22)|V |(23). e12 =h3A1 h2A2. (h1h3 h22)|H|(24). ... At this. 4 6 8 10 12 14 16 18 20 22 24 26 28 30 32 34 36 38 401.

10 Nov 2001: b = 2 (15 6) 24 = 204 (5). Substituting Equations 4 and 5 into Equation 1 we obtain. ... 8. Figure 12: Variation of forces in net cables. 24. 0 5 10 15 20 25 303.5.

17 May 2005: chosen to have a stiff-ener width of 0.06R = 24 mm, load angle γ = 7, hingeangle η = 14 and a stiffener thickness of 2 materialplies. ... This results in a plan stiffener width of22.6 mm, compared to that of 24 mm in Config VI.It also worth noting that

6 Feb 2001: b = 2 (15 6) 24 = 204 (4). Substituting Equations 3 and 4 into Equation 1 we obtain. ... 1.32. 1.29. (b). 1.48 1.24 1.24. 1.52 1.52. 3.020.43 1.40 1.40.

21 Jan 2002: 0.07 -0.06 -0.05 -0.04 -0.03 -0.02 -0.01 0 0.01-24. -20.

16 Nov 1999: c) Common limit point. 24. 5 Example of system with corner limit point; in the initial configuration p = L,ϕ = 0. ... 24. 6 Equilibrium path of simple example. 24. 7 Different shapes of equilibrium path at a corner point, for c1 6= 0 and c2 6= 0; (a)c3 6

14 May 2002: Offset 6 45.9Configuration 12 12.5(A = 1 m) 24 3.3. Table 1: Typical surface errors of reflectors with D =10 m and F = 7.8 m.

15 Aug 2003: Yee, J.C.H. and Pellegrino, S. (2003b) Folding of composite structures. Conference onDeformation and Fracture of Composites (FRC-7), Sheffield University, 22-24 April2003.

13 Sep 2000: dh = r sin ΦX ΓXY (24). dv = r (1 cos ΦX ) ΓXZ (25).

17 Feb 2006: A T300/LTM45 plain weave CFRP, 3-ply laminate (0/45/0) with uniform thickness wasadopted.Rmin was set at 24 mm, which provides a margin of 2.3 on material

9 Apr 2004: 24 and 20 into Eq. 21, and multi-plying by the arc length of the tape, Rθ. ... 24. • The steady-state moments for equal and oppositesense bending of a folded tape spring are given byEqs.

20 Mar 2006: Hence substituting Equation 23. into Equation 24, one obtains. (T1T ′̄AT3TB̄T1TC̄ T3TD̄) θA. ... 23. 7 Definition of hinge angle θA. 24. 8 Deployable square frame proposed by Hedgepeth.