diff --git a/src/solvers/indvel.m b/src/solvers/indvel.m index 98e53ffe61ae3bfc970b84e725567bac9d73c171..2f5c172d52e85ed531e4727d29f29d5d429ecd04 100644 --- a/src/solvers/indvel.m +++ b/src/solvers/indvel.m @@ -125,7 +125,7 @@ function force = coeff2force(coeff, OpRot, speed) % COEFF2FORCE Convert aerodynamic coefficient to force rho = OpRot.Op.Flow.rho; - nondim = 0.5 * rho * 2 * pi * OpRot.Rot.Bl.area .* speed.^2; + nondim = 0.5 * rho * OpRot.Rot.Bl.area .* speed.^2; force = coeff .* nondim;