Section 
                     4 Buckling strength of primary members
                  
                  
                  
                  
                  
                  
                  
                     
                        
                         
                        4.1 Application
                        
                        
                        
                        
                           
                           
                              
                              
                              4.1.1 The requirements of this Section are applicable to individual primary
                                 structural members which are subjected to axial compression or combined axial
                                 compression and bending due to overall loading.
                               
                              
                              
                            
                           
                           
                         
                        
                        
                      
                     
                   
                  
                     
                        
                         
                        4.2 Symbols
                        
                        
                        
                        
                           
                           
                              
                              
                              4.2.1 The symbols used in this Section are defined as follows:
                               
                              
                              
                              
                              
                                  ,E as defined in Pt  4, Ch  5,  3.2 Symbols
                                 
                               
                              
                              
                              
                                 
                                    
                                       
                                                  | 
                                       = | 
                                       computed axial compressive stress, in N/mm2
                                             (kgf/mm2)  | 
                                     
                                  
                               
                              
                              
                              
                                 
                                    
                                       
                                                  | 
                                       = | 
                                       computed compressive stress due to bending, in N/mm2
                                             (kgf/mm2)  | 
                                     
                                  
                               
                              
                              
                              
                              
                              
                              
                              
                              
                              
                              
                              
                              
                              
                              
                              
                                 
                                    
                                       
                                                  | 
                                       = | 
                                       local member critical buckling stress, in N/mm2
                                             (kgf/mm2)  | 
                                     
                                  
                               
                              
                              
                              
                                 
                                    
                                       
                                                  | 
                                       = | 
                                       permissible axial compressive stress, in N/mm2
                                             (kgf/mm2)  | 
                                        
                                          | = | 
                                            whichever is the lesser  | 
                                        
                                    
                                  
                               
                              
                              
                              
                                 
                                    
                                       
                                                  | 
                                       = | 
                                       permissible compressive stress due to bending, in
                                             N/mm2 (kgf/mm2)  | 
                                        
                                          | = | 
                                            whichever is the lesser  | 
                                        
                                    
                                  
                               
                              
                              
                              
                                 
                                    
                                       | 
                                                D | 
                                       = | 
                                       mean diameter of cylindrical shell, in mm  | 
                                     
                                  
                               
                              
                              
                              
                                 
                                    
                                       | 
                                                t | 
                                       = | 
                                       thickness of cylindrical shell, in mm.  | 
                                     
                                  
                               
                              
                              
                            
                           
                           
                         
                        
                        
                      
                     
                   
                  
                     
                        
                         
                        4.3 Elastic critical buckling stress
                        
                        
                        
                        
                           
                           
                              
                              
                              4.3.1 Where the elastic critical buckling stress exceeds 50 per cent of the
                                 specified minimum yield stress of the material, the calculated critical buckling
                                 stresses are to be corrected for yielding effects and are given by:
                               
                              
                              
                              
                              
                                   N/mm2 (kgf/mm2) in compression. 
                               
                              
                              
                            
                           
                           
                         
                        
                        
                      
                     
                   
                  
                     
                        
                         
                        4.4 Scantling criteria
                        
                        
                        
                        
                           
                           
                              
                              
                              4.4.1 Individual members are to be investigated for overall critical buckling
                                 in accordance with an agreed Code or Standard or  Table 5.4.1 Overall member critical
                                    buckling stress and  Table 5.4.2 Factors of safety for
                                    overall member buckling and also for local
                                 buckling.
                                 
                                  
                                    Table 5.4.1 Overall member critical
                                          buckling stress
                                    
                                       
                                          
                                             | Condition
                                                
                                              | 
                                             Member critical
                                                buckling stress
  , N/mm2 (kgf/mm2)
                                                
                                                
                                              | 
                                           
                                          
                                             (a) When λ < 
                                                
                                                
                                              | 
                                             
                                                 
                                                
                                                
                                              | 
                                           
                                          
                                             (b) When λ ≥ 
                                                
                                                
                                              | 
                                             
                                                 
                                                
                                                
                                              | 
                                           
                                          
                                             | Symbols and parameters
                                                
                                              | 
                                           
                                          
                                             
                                                 , E as defined in Pt  4, Ch  5,  3.2 Symbols
                                                
                                                
                                              | 
                                           
                                          
                                             | 
                                                l = unsupported length of member, in metres 
                                                
                                              | 
                                           
                                          
                                             | 
                                                K = effective length factor to be generally taken as
                                                unity but will be specially considered in association with end
                                                conditions 
                                                
                                              | 
                                           
                                          
                                             
                                                 = Kl = unsupported effective length of
                                                member, in metres 
                                                
                                              | 
                                           
                                          
                                             | 
                                                r = least radius of gyration of member cross-section, in
                                                mm, and may be taken as: 
                                                
                                              | 
                                           
                                          
                                             
                                                 
                                                
                                                
                                              | 
                                           
                                          
                                             | 
                                                A = cross-sectional area of member, in cm2
                                                
                                                
                                              | 
                                           
                                          
                                             | 
                                                I = least moment of inertia of member cross-section, in
                                                cm4
                                                
                                                
                                              | 
                                           
                                          
                                             | λ = slenderness ratio and may be taken as:
                                                
                                              | 
                                           
                                          
                                             
                                                 
                                                
                                                
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                                    Table 5.4.2 Factors of safety for
                                          overall member buckling
                                    
                                       
                                          
                                             | Condition
                                                
                                              | 
                                             Factor
                                                of safety, 
                                                 
                                                
                                                
                                              | 
                                           
                                          
                                             | (1) For case (a) as
                                                defined in Pt  4, Ch  5,  2.1 General:
                                                
                                              | 
                                              
                                                
                                              | 
                                           
                                          
                                             (a) When λ
                                                <  
                                                
                                                
                                              | 
                                             1,67 +  
                                                
                                                
                                              | 
                                           
                                          
                                             (b) When λ
                                                ≥  
                                                
                                                
                                              | 
                                             1,92
                                                
                                              | 
                                           
                                          
                                             | (2) For cases (b) and (c)
                                                as defined in Pt  4, Ch  5,  2.1 General:
                                                
                                              | 
                                              
                                                
                                              | 
                                           
                                          
                                             (a) When λ <  
                                                
                                                
                                              | 
                                             1,25 +  
                                                
                                                
                                              | 
                                           
                                          
                                             (b) When λ ≥  
                                                
                                                
                                              | 
                                             1,44
                                                
                                              | 
                                           
                                          
                                             | (3) For case (d) as
                                                defined in Pt  4, Ch  5,  2.1 General:
                                                
                                              | 
                                              
                                                
                                              | 
                                           
                                          
                                             (a) When λ <  
                                                
                                                
                                              | 
                                             1,0 +  
                                                
                                                
                                              | 
                                           
                                          
                                             (b) When λ ≥  
                                                
                                                
                                              | 
                                             1,15
                                                
                                              | 
                                           
                                          
                                             | Symbols and parameters
                                                
                                              | 
                                           
                                          
                                             
                                                  as defined in Pt  4, Ch  5,  4.2 Symbols
                                                
                                                
                                              | 
                                           
                                          
                                             | λ and η
                                                as defined in Pt  4, Ch  5,  4.4 Scantling criteria 4.4.1
                                                 | 
                                           
                                       
                                     
                                    
                                  
                                 
                               
                              
                              
                            
                           
                           
                           
                              
                              
                              4.4.2 The local buckling of cylindrical shells, either unstiffened or
                                 ring-stiffened, is to be investigated if the proportions of the shell conform to the
                                 following:
                               
                              
                              
                              
                              
                                  
                                 
                               
                              
                              
                            
                           
                           
                           
                              
                              
                              4.4.3 When individual primary structural members are subjected to axial
                                 compression or combined axial compression and bending, the computed design stresses
                                 are to satisfy the following requirement:
                               
                              
                              
                              
                              
                                  
                                 
                               
                              
                              
                            
                           
                           
                         
                        
                        
                      
                     
                   
                
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