Structural reliability techniques applied to plume impingement loading of the Space Station Freedom photovoltaic array

Structural Safety - Tập 15 - Trang 85-110 - 1994
Isam S. Yunis1, Kelly S. Carney1
1National Aeronautics and Space Administration, Lewis Research Center, Cleveland, OH 44135 USA

Tài liệu tham khảo

Melchers, 1987 Wirsching, 1987, An overview of reliability methods in mechanical and structural design, 260 Newell, 1989, Probabilistic structural analysis of space propulsion system turbine blades, 1860 Millwater, 1989, Structural reliability analysis using a probabilistic finite element program, 1846 Chamis, 1986, Probabilistic structural analysis methods for space propulsion system component, NASA TM-88861 Hasofer, 1974, Exact and invariant second-moment code format, J. Engrg. Mech. Div., ASCE, 100, 111, 10.1061/JMCEA3.0001848 Rackwitz, 1978, Structural reliability under combined random load sequences, Comput. Struct., 9, 489, 10.1016/0045-7949(78)90046-9 Moses, 1982, System reliability developments in structural engineering, Struct. Safety, 1, 3, 10.1016/0167-4730(82)90011-X Lazaron, 1985, Results of the SPAS-01 RCS plume impingement test, AIAA Paper 85-0407 Rayos, 1988 Carney, 1989, Free-vibration characteristics and correlation of a space station split-blanket solar array, NASA TM-101452 Timoshenko, 1961 Miller, 1977 Peery, 1982 Fu, 1990, Advanced simulation methods in system reliability, 232