An experimental study is planned to map out the low-Reynolds number incompressible steady two-dimensional aerodynamic characteristics of a promising novel airfoil. The operational parameters of the problem are the speed, density and viscosity of the freestream, the chord of the airfoil and its angle of attack. If the objective is to achieve this with the minimum number of test runs \(N_{min}\) while taking 10 equally-spaced test values of each independent parameter of the problem in a suitable range, then \(N_{min}\) is ________.