… Hi 60% 21.32 3,861 7.88 37,000 Hi 70% 20.76 3,752 7.66 36,000 7 47 -4 00 C ur re nt N ot io na l C N R P- St ru ct ur ed 74 7- 40 0 From an analysis of the results illustrated in Table … 62,840 Hi 60% 490 757 237 191 63,041 Hi 70% 490 757 238 191 63,242 C ur re nt 7 47 -4 00 N ot io na l C N R P- St ru ct ur ed 74 7- 40 0 The high mass CNRP-structured aircraft stalls at … Nanotechnology, Vol. 9, pp. 184-191. 20. Frankland, S. J. V., T. Bandorawalla, and T. S. Gates, 2003, “Calculation of Non-Bonded Forces Due to Sliding of Bundled Carbon Nanotubes,” Paper …