1 Minimum Power Assessment is based on the solution of a one degree-of-freedom
                           manoeuvring equation in longitudinal direction to demonstrate that the ship can move
                           with the speed of 2.0 knots through water in wind and wave directions from head to
                           30 degrees off-bow for a situation of weather vaning. The assessment consists of the
                           following steps: 
                        
                        
                        
                        
                           - 
                              
                              
                              .1 calculate the maximum total resistance in the longitudinal ship direction
                                 over wind and wave directions from head to 30 degrees off-bow; 
                               
- 
                              
                              
                              .2 calculate corresponding required brake power and rotation speed of the
                                 installed engine, considering the resistance and propulsion characteristics
                                 of the ship including appendages; and 
                               
- 
                              
                              
                              .3 check whether the required brake power does not exceed the maximum
                                 available brake power of the installed engine, defined according to the
                                 engine manufacturer data at the actual rotation speed of the installed
                                 engine. 
                               
2 The maximum total resistance is defined as sum of the resistance in calm-water at
                           the 2.0 knots forward speed U and the maximum added resistance in seaway
                           Xa over wind and wave directions from head to 30 degrees off-bow. 
                        
                        
                        
                        
                        Requirement 
                        
                        
                        
                        3 To satisfy the requirements of Minimum Power Assessment, the required brake power  in the adverse conditions at the forward speed 2.0
                           knots through water should not exceed the available brake power of the installed
                           engine
 in the adverse conditions at the forward speed 2.0
                           knots through water should not exceed the available brake power of the installed
                           engine  in the same conditions:
 in the same conditions:
                        
                        
                        
                        
                         ≤
 ≤ 
                        
                        
                        
                        4 The required brake power  is calculated as
 is calculated as
                        
                        
                        
                        
                           - 
                              
                              
                               
 
- 
                              
                              
                              where 
- 
                              
                              
                              
                                 
                                    
                                       
                                          | nP (1/s) | is the propeller rotation rate in
                                             the specified adverse conditions and the specified forward
                                             speed; |  
                                          | Q (N⋅m) | is the corresponding propeller
                                             torque; |  
                                          | ηs | is the mechanical transmission
                                             efficiency of the propeller shaft, approved for the EEDI
                                             verification; |  
                                          | ηg | is the gear efficiency, approved
                                             for the EEDI verification; and |  
                                          | ηR | is the relative rotative
                                             efficiency. |  
 
 
5 The available brake power  in the adverse conditions at the forward speed is
                           defined as the maximum engine output at the actual rotation speed, taking into
                           account maximum torque limit, surge/air limit and all other relevant limits in
                           accordance with the engine manufacturer's data.
 in the adverse conditions at the forward speed is
                           defined as the maximum engine output at the actual rotation speed, taking into
                           account maximum torque limit, surge/air limit and all other relevant limits in
                           accordance with the engine manufacturer's data.
                        
                        
                        
                        
                        Definition of propulsion point
                        
                        
                        
                        6 The propeller rotation rate nP and the corresponding
                           propeller advance ratio J in the adverse conditions at the forward speed are defined
                           from the propeller open-water characteristics by solving the following equation:
                        
                        
                        
                        
                           - 
                              
                              
                               
 
- 
                              
                              
                              where 
- 
                              
                              
                              
                                 
                                    
                                       
                                          | KT | is the thrust coefficient of the
                                             propeller, defined from the propeller open-water
                                             characteristics; |  
                                          | T (N) | is the required propeller
                                             thrust; |  
                                          | ρ (kg/m3) | is the sea water density, ρ = 1025
                                             kg/m3; |  
                                          | ua (m/s) | is the propeller advance speed;
                                             and |  
                                          | DP (m) | is the propeller diameter. |  
 
 
7 The corresponding torque of the propeller is calculated as
                        
                        
                        
                           - 
                              
                              
                               
 
- 
                              
                              
                              where 
- 
                              
                              
                              
                                 
                                    
                                       
                                          | KQ | is the torque coefficient of the
                                             propeller, defined from the propeller open-water
                                             characteristics. |  
 
 
8 The propeller advance speed ua is calculated as
                        
                        
                        
                        
                           - 
                              
                              
                              ua = U(1 − w)
                               
- 
                              
                              
                              where 
- 
                              
                              
                              
                                 
                                    
                                       
                                          | U (m/s) | is the forward speed 2.0 knots
                                             through water; and |  
                                          | W | is the wake fraction. |  
 
 
Definition of required propeller thrust
                        
                        
                        
                        9 The required propeller thrust T is defined from the equation
                        
                        
                        
                           - 
                              
                              
                               
 
- 
                              
                              
                              where 
- 
                              
                              
                              
                                 
                                    
                                       
                                          | Xs (N) | is the resistance in calm-water at
                                             the forward speed including resistance due to
                                             appendages; |  
                                          | Xa (N) | is the maximum added resistance in
                                             seaway Xa; and |  
                                          | t | is the thrust deduction factor
                                             taking into account suction force on the ship hull due to
                                             propeller thrust. |  
 
 
Definition of calm water characteristics 
                        
                        
                        
                        10 The calm-water characteristics used for the assessment, such as calm-water
                           resistance, self-propulsion factors and propeller open-water characteristics, are
                           defined by the methods approved for EEDI verification, including: 
                        
                        
                        
                        
                           - 
                              
                              
                              .1 the calm-water resistance Xs, defined from the
                                 following equation: 
                               Xs = (1 + k)CF1 ρSU2 ρSU2
 where k is the form factor, CF is the frictional resistance
                                 coefficient, ρ is sea water density, ρ = 1025 kg/m3, S is the
                                 wetted surface area of the hull and the appendages and U is the forward
                                 speed; 
                               .2 the thrust deduction factor t and wake fraction w at the forward speed and
                                 relative rotative efficiency ηR. Default conservative estimate may also be
                                 used for thrust deduction factor and wave fraction; t=0.1 and w=0.15
                                 respectively; and 
                               .3 the propeller open-water characteristics KT(J) and
                                 KQ(J).
                               
Definition of added resistance 
                        
                        
                        
                        11 The maximum added resistance in seaway Xa is defined as sum of maximum
                           added resistance due to wind Xw, maximum added resistance due to waves
                           Xd and maximum added rudder resistance due to manoeuvring in seaway
                           Xr over wind and wave directions from head to 30 degrees off-bow. 
                        
                        
                        
                        
                        Definition of wind resistance 
                        
                        
                        
                        12 The maximum added resistance due to wind Xw is calculated as
                        
                        
                        
                           - 
                              
                              
                               
 
- 
                              
                              
                              where 
- 
                              
                              
                              
                                 
                                    
                                       
                                          |   | is the non-dimensional aerodynamic
                                             resistance coefficient; |  
                                          | ε (degree) | is the apparent wind angle; |  
                                          | ρa
                                             (kg/m3) | is the air density,
                                             ρa=1.2 kg/m3; |  
                                          | vwr (m/s) | is the relative wind speed,
                                             vwr=U + vwcosμ; |  
                                          | vw (m/s) | is the absolute wind speed, defined
                                             by the adverse conditions in paragraph 1 of these
                                             guidelines; and |  
                                          | AF
                                             (m2) |  |  
 
 
13 The maximum added resistance due to wind Xw is defined as maximum over
                           wind directions from head ε=0 to 30 degrees off-bow ε=30. 
                        
                        
                        
                        
                        14 The non-dimensional aerodynamic resistance coefficient  is defined from wind tunnel tests or equivalent
                           methods verified by the Administrations or the Recognized Organizations.
                           Alternatively, it can be assumed with
 is defined from wind tunnel tests or equivalent
                           methods verified by the Administrations or the Recognized Organizations.
                           Alternatively, it can be assumed with  = 1.1, as the maximum over wind directions from head
                           to 30 degrees off-bow. If deck cranes are installed in the ship and the lateral
                           projected area of the deck cranes is equal to or exceeds 10% of the total lateral
                           projected area above the waterline of the ship,
 = 1.1, as the maximum over wind directions from head
                           to 30 degrees off-bow. If deck cranes are installed in the ship and the lateral
                           projected area of the deck cranes is equal to or exceeds 10% of the total lateral
                           projected area above the waterline of the ship,  =1.4 should be assumed instead of
=1.4 should be assumed instead of  =1.1.
=1.1.
                        
                        
                        
                        
                        Definition of added resistance due to waves 
                        
                        
                        
                        15 The maximum added resistance due to waves Xd is defined in accordance with either 
                        
                        
                        
                           - 
                              
                              
                              .1 expression 
- 
                              
                              
                              .2 or spectral method 
16 The maximum added resistance due to waves Xd is defined as
                           maximum over wave directions from head μ=0 to 30 degrees off-bow μ=30. The range of
                           peak wave periods TP applied in the assessment is from 3.6
                            to the greater one of 5.0
 to the greater one of 5.0 or 12.0 seconds, with the step of peak wave period
                           not exceeding 0.5 seconds.
 or 12.0 seconds, with the step of peak wave period
                           not exceeding 0.5 seconds.
                        
                        
                        
                        
                        17 The added resistance in short-crested irregular head waves may be regarded as the
                           maximum added resistance over wave directions from head to 30 degrees off-bow,
                           because in short-crested waves, the maximum added resistance over wave directions
                           from head waves to 30 degrees off-bow occurs in head waves.
                        
                        
                        
                        
                        18 The spreading function D(μ−μ′) is defined as cos2-directional
                           spreading. Alternatively, long-crested seaway may be assumed with D(μ−μ′) = 1; in
                           this case, the maximum added resistance due to waves Xd can be determined
                           by multiplying the added resistance in long-crested irregular head waves by the
                           correction factor 1.3, to consider that maximum of the added resistance in
                           long-crested waves does not always correspond to head wave direction. 
                        
                        
                        
                        
                        19 The quadratic transfer functions of added resistance in regular waves
                            are defined from seakeeping tests or equivalent
                           methods verified by the Administrations or the Recognized Organizations.
                           Alternatively, the semi-empirical method specified in appendix of this document can
                           be used.
 are defined from seakeeping tests or equivalent
                           methods verified by the Administrations or the Recognized Organizations.
                           Alternatively, the semi-empirical method specified in appendix of this document can
                           be used. 
                        
                        
                        
                        
                        Definition of added rudder resistance due to manoeuvring in seaway 
                        
                        
                        
                        20 The maximum additional rudder resistance due to manoeuvring in seaway
                           Xr may be calculated for practicality in a simplified way as 
                        
                        
                        
                        
                        Xr=0.03 · Ter, where Ter is the propeller thrust
                           excluding Xr from T.
                        
                        
                        
                      
                     
                     
                     
                        APPENDIX TO APPENDIX 2 - SEMI-EMPIRICAL METHOD FOR QUADRATIC TRANSFER FUNCTIONS
                           OF ADDED RESISTANCE IN REGULAR WAVES
                        
                        
                        
                        
                        The method for the calculation of the quadratic transfer functions of added
                           resistance give in this appendix can be applied to wave directions from head to
                           beam. Therefore, this method can be used for obtaining the added resistance in
                           short-crested irregular waves of the head mean wave direction.
                        
                        
                        
                        
                        The quadratic transfer functions of added resistance in regular head to beam waves
                           X′d= , N/m2, can be calculated as a sum
, N/m2, can be calculated as a sum
                        
                        
                        
                        
                        X′d = X′dM + X′dR
                        
                        
                        
                        of X′dM, the component of added resistance due to motion (radiation)
                           effect, and X′dR, the component of added resistance due to reflection
                           (diffraction) effect in regular waves.
                        
                        
                        
                        
                        The expression of X′dM is given as follows:
                        
                        
                        
                        
                        
                        
                        
                        
                        where
                        
                        
                        
                        
                        
                        
                        
                        
                        
                        
                        
                        
                        
                        
                        
                        
                        
                        
                        The expression of X′dR is given as follows:
                        
                        
                        
                        
                        
                        
                        
                        where
                        
                        
                        
                           - 
                              
                              
                               is the added resistance due to
                                 reflection/diffraction effect of the Siwaterline segment,
                                 as shown in Figure 1. is the added resistance due to
                                 reflection/diffraction effect of the Siwaterline segment,
                                 as shown in Figure 1.
 
- 
                              
                              
                               
 Figure 1: Sketch of the waterline profile of a ship and related
                                 definitions
                               when E1≤ β ≤ π 
- 
                              
                              
                               
 
- 
                              
                              
                              when π-E1 ≤ β ≤ π 
- 
                              
                              
                               
 
- 
                              
                              
                              when 0 ≤ β ≤ π-E2 
- 
                              
                              
                               
 
- 
                              
                              
                              when 0 ≤ β ≤ E2 
- 
                              
                              
                               
 
- 
                              
                              
                              where 
- 
                              
                              
                                 - 
                                    
                                    
                                    
                                       
                                          
                                             
                                                | ω0 | is the
                                                   frequency of the incident wave; |  
                                                |   | is the draft
                                                   coefficient, calculated as |  
 
 
 
- 
                              
                              
                               
 where for S1 and S2 segments
                               and for S3 and S4 segments
                                
 f(β) = 