Geometric Nonlinear Analyses for Large Space Frames Considering Thermal-Structural Coupling

2007 ◽  
Vol 31 (1) ◽  
pp. 40-58 ◽  
Author(s):  
Jin Duan ◽  
Zhi-Hai Xiang ◽  
Ming-De Xue
2007 ◽  
Vol 24 (4) ◽  
pp. 407-431 ◽  
Author(s):  
Ean Tat Ooi ◽  
Sellakkutti Rajendran ◽  
Joon Hock Yeo

2011 ◽  
Vol 38 (8) ◽  
pp. 553-559 ◽  
Author(s):  
Carlos A. Almeida ◽  
Juan C.R. Albino ◽  
Ivan F.M. Menezes ◽  
Glaucio H. Paulino

1993 ◽  
pp. 1: 497-506 ◽  
Author(s):  
Tsuneyoshi Nakamura ◽  
Makoto Ohsaki
Keyword(s):  

2011 ◽  
Vol 11 (05) ◽  
pp. 929-947 ◽  
Author(s):  
K. J. R. RASMUSSEN ◽  
B. P. GILBERT

The paper presents a study of the capacities of steel rack frames based on linear analysis (LA), geometric nonlinear analysis (GNA), and geometric and material nonlinear analysis (GMNIA). In the case of linear and geometric nonlinear analyses, the design is carried out to the Australian cold-formed steel structures AS/NZS4600. The study includes braced, unbraced, and semi-braced frames, and compact and noncompact cross sections. The paper shows axial force and bending moment paths for geometric and geometric and material nonlinear analyses, and explains the differences observed in the design capacities obtained using the different types of analysis based on these paths. The paper provides evidence to support the use of advanced GMNIA for the direct design of steel rack frames without the need for checking section or member capacities to a structural design standard.


1993 ◽  
pp. 1: 369-377
Author(s):  
H. Kato ◽  
T. Kawazoe ◽  
I. Kubodera ◽  
F. Matsushita
Keyword(s):  

1997 ◽  
Vol 161 ◽  
pp. 761-776 ◽  
Author(s):  
Claudio Maccone

AbstractSETI from space is currently envisaged in three ways: i) by large space antennas orbiting the Earth that could be used for both VLBI and SETI (VSOP and RadioAstron missions), ii) by a radiotelescope inside the Saha far side Moon crater and an Earth-link antenna on the Mare Smythii near side plain. Such SETIMOON mission would require no astronaut work since a Tether, deployed in Moon orbit until the two antennas landed softly, would also be the cable connecting them. Alternatively, a data relay satellite orbiting the Earth-Moon Lagrangian pointL2would avoid the Earthlink antenna, iii) by a large space antenna put at the foci of the Sun gravitational lens: 1) for electromagnetic waves, the minimal focal distance is 550 Astronomical Units (AU) or 14 times beyond Pluto. One could use the huge radio magnifications of sources aligned to the Sun and spacecraft; 2) for gravitational waves and neutrinos, the focus lies between 22.45 and 29.59 AU (Uranus and Neptune orbits), with a flight time of less than 30 years. Two new space missions, of SETI interest if ET’s use neutrinos for communications, are proposed.


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