2 structure design loads
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CALCULATING WIND LOADS ON LOW-RISE STRUCTURES PER …
www.awc.orgC1.1.2 Design Loads Unless stated otherwise, all calculations are based on standard linear elastic analysis and Allowable Stress Design (ASD) load combinations using loads from ASCE 7-10 Minimum Design Loads for Buildings and Other Structures. Dead Loads Unless stated otherwise, tabulated values assume the following dead loads: Roof pf10 psf
DESIGN RECOMMENDATION FOR STORAGE TANKS AND …
www.aij.or.jp3.2 Dead Loads ----- 9 3.3 Live Loads ----- 9 ... Qd design yield shear force at the base of the structure (N) Qdi design shear force imposed just below the i-th mass in case that the structure is
Chapter 2 Aircraft Structure
mae.ufl.edu2-3 Figure 2-4. Airplane components. Figure 2-5. Truss-type fuselage structure. Figure 2-3. Center of gravity (CG). Major Components Although airplanes are designed for a variety of purposes, most of them have the same major components. [Figure 2-4] The overall characteristics are largely determined by the original design objectives.
Topic 14 - Foundation Design - Memphis
www.ce.memphis.eduInstructional Materials Complementing FEMA 451, Design Examples Foundation Design 14-38 Tie Between Pile Caps (2) #6 top bars (3) #6 bottom bars #4 ties at 7" o.c. 2" clear at sides 3" clear at top and bottom •Designed for axial force (+/-) •Pile cap axial load times S DS/10 •Often times use grade beams or thickened slabs one grade