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18 May 2007: σaxial [MPa]. t = 1 x 10-20. t = 4 x 10-20 s. ... 13 of 15. American Institute of Aeronautics and Astronautics. -20 -15 -10 -5 0 5.

8 Feb 2000: u v = 2. h 2. 24. L. h. 2(19). u2 v2 =. h 2. 24. 2 L. h. 4B2 2. 4(20). Substituting back into Equation 18, ignoring higherorder terms, and ... n32to. obtain. R0=. 1p2LK. (33). 0.20. 0.20.4. 0.60.8. 11.2. -0.4. -0.2 0.

14 Mar 2003: g7 =1. 2wH 20. (. 2 sin φ0 5 sin3 φ0 3 sin5 φ0). ... 20). Further consideration must be given to the location of trun-cation node D.

3 Jun 2002: ξ =γ. 2+. 12. (w. ξ. )2(20). Thus, ξ also is not constant, and hence the average strain energy ofstretching, Us, over a wrinkle is given by. ... 20, 200–207, 227–233, 256–262, 279-284. Wong,Y.W. (2000) Analysis of Wrinkle Patterns in

5 Apr 2007: idth. [N. /mm. ]εx [%]. 0 0.2 0.4 0.6 0.8 1 1.20. ... The distance between the outer supports was60 mm and the distance between the inner supports 20 mm.

13 Sep 2000: l2. l2. [M ]T [K]T [M ] ds. ). 2g (20). ... 10. 20. 30. 40. 50. 60. 70. 80. 90. 100. 0.03 0.02 0.01 0 0.01 0.02 0.03 0.04 0.050.03.

22 May 2003: g7 =1. 2wH 20. (. 2 sin φ0 5 sin3 φ0 3 sin5 φ0). ... 20). Further consideration must be given to the location of trun-cation node D.

14 Feb 2003:  θB0. = [0](20). At first glance, the matrix equation (20) would ap-pear to be equivalent to 9 scalar equations in 4 un-knowns, not 16, since the 7 equations

20 Jul 2007: glass-covered surface, Int. Journal of Space Structures vol. 20, No. 1,2005[3].

16 Nov 1999: ϕ1+ 180 [o]. p. 180. [o]. L1. L2. Snap. Snap. 0 20 40 60. ... are shown flat for clarity. 20. 2 Antenna deployment. 21. 3 Simulation model.