diff --git a/src/classes/@ElemPerf/ElemPerf.m b/src/classes/@ElemPerf/ElemPerf.m
index 8f883c8f24199a69fc34e46845f98e56998cbdb9..75b9a602e2d79c647f09530bdb0dca24304d07bb 100644
--- a/src/classes/@ElemPerf/ElemPerf.m
+++ b/src/classes/@ElemPerf/ElemPerf.m
@@ -96,7 +96,7 @@ classdef ElemPerf < handle
     % Cache for dependent properties to avoid excessive recalculation
     properties (Access = private, Hidden)
         alpha_    (1, :) double % Angle of attack, [rad]
-        reynolds_    (1, :) double % Reynolds number, [-]
+        reynolds_ (1, :) double % Reynolds number, [-]
         indVelAx_ (1, :) double % Induced axial velocity at rotor disk, [m/s]
         indVelTg_ (1, :) double % Induced tangential velocity at rotor disk, [m/s]
         inflowRat_ (1, :) double % Inflow ratio, [-]
@@ -160,9 +160,8 @@ classdef ElemPerf < handle
         end
 
         function reynolds = get.reynolds(self)
-            % if true reynolds is unknown, we use an approximated value
-            % with the upstream velocity instead of relative velocity at
-            % the rotor disk
+            % If Reynolds in unknown, we use an approximate solution
+            % neglecting induced velocities.
             if isempty(self.reynolds_)
                 relVel = sqrt(self.tgSpeed.^2 + self.upstreamVelAx.^2);
                 reynolds = Flow.reynolds(relVel, Rot.Bl.chord, Op.Flow.mu, Op.Flow.rho);
@@ -207,7 +206,6 @@ classdef ElemPerf < handle
         end
 
         function set.reynolds(self, val)
-            % Cache value
             self.reynolds_ = val;
         end