Section 
                     5 Shell envelope framing
                  
                  
                  
                  
                  
                  
                  
                     
                        
                         
                        5.1 Side structure
                        
                        
                        
                        
                           
                           
                              
                              
                              5.1.1 The
                                 scantlings of frames, or side longitudinals, web frames or transverses,
                                 and stringers below 1,6T above base are to satisfy the
                                 requirement of Pt  4, Ch  1 General Cargo Ships and this
                                 Section, but may be required to be confirmed by direct calculation.
                                 The scantlings of these members above 1,6T from base
                                 may require special consideration on the basis of the particular structural
                                 arrangements, design deck loading, hull vertical bending stresses,
                                 and position of the member above the waterline.
                                 
                               
                              
                              
                            
                           
                           
                           
                              
                              
                              5.1.2 The
                                 scantlings of side transverses supporting shell longitudinals above
                                 1,6T are to satisfy the requirements of:
                                 
                               
                              
                              
                              
                                 - 
                                    
                                    
                                    
                                       Pt  4, Ch  1,  6 Shell envelope framing, Pt  3, Ch  5,  4 Shell envelope framing and Pt  3, Ch  6,  4 Shell envelope framing.
                                       
                                     
                                    
                                    
                                  
                                 - 
                                    
                                    
                                    
The minimum geometric
                                       properties required in order to provide rotational constraint to the
                                       end of the deck transverse in way:
                                     
                                    
                                    
                                    
                                    
                                  
                               
                              
                              
                              
                              but is not to be less than 0,339S k P
                                 s 
                                 L
                                 d
                                 2 cm3
                                 
                               
                              
                              
                              
                              
                                  
                                 s is not to be less than  
                                 d
                                   cm4
                                 
                               
                              
                              
                              
                                 
                                    where
                                    
                                       | 
                                                
                                             P
                                             s
                                              | 
                                       = | 
                                       deck design loading, in kN/m2, see 
                                             Table 2.3.1 Design deck loadings (ferries and
                                                passenger ships only)
                                              | 
                                     
                                    
                                       | 
                                                
                                             L
                                             d
                                              | 
                                       = | 
                                       span of adjacent deck transverse, in metres | 
                                     
                                    
                                       | 
                                                
                                             Z
                                             d
                                              | 
                                       = | 
                                       actual modulus of adjacent deck transverse, in cm3
                                              | 
                                     
                                    
                                       | 
                                                
                                             Z
                                             dR
                                              | 
                                       = | 
                                       Rule modulus of adjacent deck transverse, in cm3
                                              | 
                                     
                                    
                                       
                                                
                                              
                                             d
                                              | 
                                       = | 
                                       moment of
                                             inertia of adjacent deck transverse, in cm4
                                              | 
                                     
                                    
                                       | 
                                                
                                             L
                                             s
                                              | 
                                       = | 
                                       span of side shell transverse, in metres | 
                                     
                                    
                                       
                                                
                                              
                                             s
                                              | 
                                       = | 
                                       moment of
                                             inertia of side shell transverse, in cm4
                                              | 
                                     
                                    
                                       | 
                                                
                                             S, k
                                              | 
                                       = | 
                                       as defined in Pt  4, Ch  2,  1.5 Symbols 1.5.1
                                              | 
                                     
                                    
                                       | 
                                                 | 
                                       = | 
                                       Due account should be taken of the shell window dimensions when
                                             determining the effective width of attached plating. | 
                                     
                                  
                               
                              
                              
                            
                           
                           
                           
                              
                              
                              5.1.3 The
                                 required modulus of transverse main and 'tween deck frames, which
                                 may have reasonably constant convex curvature over their entire length,
                                 may be corrected for curvature as follows:
                               
                              
                              
                              
                                 
                                    
                                       | 
                                                
                                             Z
                                             min
                                              | 
                                       = | 
                                       
                                             Z
                                             rule
                                               cm3
                                              | 
                                     
                                  
                               
                              
                              
                              
                              
                              
                              
                              
                                 
                                  
                                 
                                 Figure 2.5.1 Distance between span support points and curvature
                               
                              
                              
                            
                           
                           
                           
                           
                              
                              
                              5.1.4 Where
                                 ramp openings are fitted adjacent to the ship’s side, adequate
                                 support for the side framing is to be provided.
                               
                              
                              
                            
                           
                           
                         
                        
                        
                      
                     
                   
                  
                     
                        
                         
                        5.2 Strengthening for wave impact loads
                        
                        
                        
                        
                           
                           
                              
                              
                              5.2.1 The
                                 side structure in the forward and after portions of the hull is to
                                 be strengthened against bow flare or wave impact pressure. Typically,
                                 strengthening is to be considered over the following areas:
                               
                              
                              
                              
                                 - over the after body in way of a flat counter stern which is close
                                    to the waterline.
                                 
 
                                 - over the fore end side and bow structure above the waterline and
                                    up to the deck at side.
                                 
 
                                 - other areas where the hull exhibits significant flare.
 
                               
                              
                              
                            
                           
                           
                           
                              
                              
                              5.2.2 The
                                 scantlings of secondary stiffeners are not to be less than:
                               
                              
                              
                              
                                 - 
                                    
                                    
                                    
Effective plastic
                                       section modulus of stiffeners:
                                     
                                    
                                    
                                    
                                       
                                          
                                             | 
                                                      
                                                   Z
                                                   p
                                                    | 
                                             = | 
                                              3,75h
                                                   s 
                                                   s
                                                   cm 
                                                   kl
                                                   e
                                                   2 x 10–3 cm3
                                                    | 
                                           
                                        
                                     
                                    
                                    
                                    
                                    
                                    
                                    
                                    Other symbols are as defined in Pt  4, Ch  2,  1.5 Symbols 1.5.2.
                                       
                                     
                                    
                                    
                                  
                                 - 
                                    
                                    
                                    
Web area of secondary
                                       stiffeners
                                     
                                    
                                    
                                    
                                       
                                          
                                             | 
                                                      
                                                   A
                                                    | 
                                             = | 
                                             3,7s
                                                   cm 
                                                   k h
                                                   s 
                                                     x 10–4 cm2
                                                    | 
                                           
                                        
                                     
                                    
                                    
                                  
                               
                              
                              
                              
                              where 
                              
                              
                              
                              
                              
                              
                              
                              
                              
                              Other symbols are as defined in Pt  4, Ch  2,  1.5 Symbols 1.5.2.
                                 
                               
                              
                              
                            
                           
                           
                           
                              
                              
                              5.2.3 The
                                 effective section properties of secondary stiffeners are to be taken
                                 as:
                               
                              
                              
                              
                                 - 
                                    
                                    
                                    
Plastic section
                                       modulus of secondary stiffeners, Z
                                       p, is to
                                       be taken as:
                                       
                                     
                                    
                                    
                                  
                               
                              
                              
                              
                                 
                                    
                                       | 
                                                
                                             Zp
                                              | 
                                       = | 
                                       (2,8 x 10-4 scm
                                             tp2) - (10-3
                                             bf
                                             bfc
                                             tf sinθe) +(5 x 10-4
                                             (hw2
                                             tw + 2bf
                                             tf
                                             hw) cosθe) cm3 | 
                                     
                                  
                               
                              
                              
                              
                                 
                                    where
                                    
                                       | 
                                                θe
                                              | 
                                       = | 
                                       
                                             C
                                             0 (90 – φ)
                                              | 
                                     
                                    
                                       | 
                                                
                                             Co
                                              | 
                                       = | 
                                       1,1 | 
                                     
                                    
                                       | 
                                                φ | 
                                       = | 
                                       the angle
                                             between the stiffener and the side shell, in degrees | 
                                     
                                    
                                       | 
                                                
                                             b-fc
                                              | 
                                       = | 
                                       0,5 (b
                                             f – t
                                             w)
                                             for L profiles
                                              | 
                                        
                                          | = | 
                                          0 for flat bar and T profiles | 
                                        
                                       
                                          | = | 
                                            for bulb profiles, see
                                                Figure 4.7.1 Dimensions of longitudinals in Pt  3, Ch  4 Longitudinal Strength, for c | 
                                        
                                    
                                    
                                       | 
                                                
                                             h
                                             w
                                              | 
                                       = | 
                                       height of stiffener web, in mm | 
                                     
                                    
                                       | 
                                                
                                             t
                                             w
                                              | 
                                       = | 
                                       web thickness, in mm | 
                                     
                                    
                                       | 
                                                
                                             b
                                             f
                                              | 
                                       = | 
                                       breadth of flange, in mm | 
                                     
                                    
                                       | 
                                                
                                             t
                                             f
                                              | 
                                       = | 
                                       flange thickness, in mm | 
                                     
                                    
                                       | 
                                                
                                             t
                                             p
                                              | 
                                       = | 
                                       thickness of attached plating, in mm | 
                                     
                                  
                               
                              
                              
                              
                                 - 
                                    
                                    
                                    
Web area of secondary stiffeners, A
                                       s, is to be taken as:
                                       
                                     
                                    
                                    
                                  
                               
                              
                              
                              
                                 
                                    
                                       | 
                                                
                                             A
                                             s
                                              | 
                                       = | 
                                       0,01 (h
                                             w + t
                                             p) t
                                             w sinφ cm2
                                              | 
                                     
                                  
                               
                              
                              
                            
                           
                           
                           
                              
                              
                              5.2.4 Where
                                 the stiffener web is not perpendicular to the plating, tripping brackets
                                 have to be fitted in order to obtain adequate lateral stability.
                               
                              
                              
                            
                           
                           
                           
                              
                              
                              5.2.5 The
                                 scantlings of primary members are not to be less than:
                               
                              
                              
                              
                                 - 
                                    
                                    
                                    
Section modulus
                                       of primary members
                                     
                                    
                                    
                                    
                                       
                                          
                                             | 
                                                      
                                                   Z
                                                    | 
                                             = | 
                                             2 γz 
                                                   k h
                                                   s 
                                                   q v 
                                                    
                                                   e
                                                   2 cm3
                                                    | 
                                           
                                        
                                     
                                    
                                    
                                  
                                 - 
                                    
                                    
                                    
Web area of primary
                                       members
                                     
                                    
                                    
                                    
                                       
                                          
                                             | 
                                                      
                                                   A
                                                    | 
                                             = | 
                                             0,2 γA 
                                                   k h
                                                   s 
                                                   q v 
                                                    
                                                   e cm2
                                                    | 
                                           
                                        
                                     
                                    
                                    
                                    
                                    
                                    
                                  
                               
                              
                              
                              
                              γA and γZ are strength factors
                                 dependent on the load position
                                 
                               
                              
                              
                              
                              for q <
                                 1 γA = q
                                 3 – 2q
                                 2 + 2 and γZ = 3q
                                 3 –
                                 8q
                                 2 + 6q
                                  for q =
                                 1 γA = 1 and γZ = 1
                                 
                               
                              
                              
                              
                              
                                 
                                    
                                       | 
                                                
                                             q
                                              | 
                                       = | 
                                       
                                              but ≤ 1
                                              | 
                                     
                                  
                               
                              
                              
                              
                              for web frames: 
                              
                              
                              
                                 
                                    
                                       | 
                                                
                                             u
                                              | 
                                       = | 
                                       is the minimum of g
                                             bfv or  
                                             e
                                              | 
                                     
                                  
                               
                              
                              
                              
                                 
                                    
                                       | 
                                                
                                             v
                                              | 
                                       = | 
                                       is the minimum of g
                                             bfh or S
                                             cm
                                              | 
                                     
                                  
                               
                              
                              
                              
                              for primary stringers: 
                              
                              
                              
                                 
                                    
                                       | 
                                                
                                             u
                                              | 
                                       = | 
                                       is the minimum of g
                                             bfh or  
                                             e
                                              | 
                                     
                                  
                               
                              
                              
                              
                                 
                                    
                                       | 
                                                
                                             v
                                              | 
                                       = | 
                                       is the minimum of g
                                             bfv or S
                                             cm
                                              | 
                                     
                                  
                               
                              
                              
                              
                              
                              
                              
                                 - 
                                    
                                    
                                    
The web of the
                                       primary member is to be adequately stiffened.
                                     
                                    
                                    
                                  
                               
                              
                              
                              
                              
                                 
                                  
                                 
                                 Figure 2.5.2 Mean spacing between primary members, S
                                       cm,
                                       and the extents of wave impact pressure g
                                       bfh and g
                                       bfv
                                       
                               
                              
                              
                            
                           
                           
                           
                           
                              
                              
                              5.2.6 The
                                 extents of the wave impact pressure are to be derived as follows:
                               
                              
                              
                              
                                 - 
                                    
                                    
                                    
the vertical extent, g
                                       bfv, is to be taken as:
                                       
                                     
                                    
                                    
                                    
                                    
                                  
                                 - 
                                    
                                    
                                    
the horizontal
                                       extent, g
                                       bfh, is to be taken as:
                                       
                                     
                                    
                                    
                                    
                                    
                                    
                                    
                                    
                                    
                                  
                               
                              
                              
                            
                           
                           
                           
                              
                              
                              5.2.7 For
                                 primary members with cut-outs for the passage of secondary stiffeners,
                                 and which may have web stiffeners connected to the secondary stiffener,
                                 buckling checks are to be carried out to ensure that the primary member
                                 web plating and web stiffener will not buckle under the design load.
                                 The buckling procedure to be followed is given in Table 5.1.3 Buckling procedure for primary
                                    member web plating and web stiffener in Pt  3, Ch  5 Fore End Structure. Where the web stiffener is
                                 fitted with a bracket, the buckling capability of the web stiffener
                                 in way of the cut-out is to take account of the bracket. Where no
                                 web stiffener is fitted, the buckling capability of the primary member
                                 web plating is to be checked for the total load transmitted to the
                                 connection.
                                 
                               
                              
                              
                            
                           
                           
                           
                              
                              
                              5.2.8 Where
                                 the angle between primary structure web and the plating is less than
                                 70°, the effective section modulus and shear area are to take
                                 account of the non-perpendicularity.
                               
                              
                              
                            
                           
                           
                           
                              
                              
                              5.2.9 The
                                 structural scantlings required in areas strengthened against bow flare
                                 slamming are to be tapered to meet the normal shell envelope requirements.
                               
                              
                              
                            
                           
                           
                           
                           
                           
                         
                        
                        
                      
                     
                   
                
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