LaRC design analysis report for National Transonic Facility for 9% nickel tunnel shell. Volume 2: Finite element analysis of corners 3 and 4
For abstract, see N76-33543.
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For abstract, see N76-33543.
For abstract, see N76-33543.
For abstract, see N76-33543.
For abstract, see N76-33543.
For abstract, see N76-33543.
The results of extensive computer (finite element, finite difference and numerical integration), thermal, fatigue, and special analyses of critical portions of a large pressurized, cryogenic wind tunnel (National Transonic Facility) are presented. The computer models, loading and boundary conditions are described. Graphic capability was used to display model geometry, section properties, and stress results. A stress criteria is presented for evaluation of the results of the analyses. Thermal analyses were performed for major critical and typical areas. Fatigue analyses of the entire tunnel circuit are presented.
For abstract, see N76-33552.
For abstract, see N76-33552.
For abstract, see N76-33552.
For abstract, see N76-33552.
For abstract, see N76-33552.
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