Sensitivity analysis for the Navier-Stokes equations with two-equation turbulence models

Aerodynamic sensitivity analysis is performed for the Navier-Stokes equatio ns, coupled with two-equation turbulence. models using a discrete adjoint m ethod and a direct differentiation method, respectively. Like the mean flow equations, the turbulence model equations are also hand differentiated to calculate accurately the sensitivity derivatives of how quantities with res pect to design variables in turbulent viscous hows. Both the direct differe ntiation code and the adjoint variable code adopt the same time integration scheme with the Row solver to solve the differentiated equations efficient ly. The sensitivity codes are then compared with the flow solver in terms o f solution accuracy, computing time, and computer memory requirements. The sensitivity derivatives obtained from the sensitivity codes with different turbulence models are compared with each other. Using two-equation turbulen ce models, it is observed that a usual assumption of constant turbulent edd y viscosity in adjoint methods may lead to inaccurate results in a case of turbulent hows involving strong shocks, The capability of the present sensi tivity codes to treat complex geometry is successfully demonstrated by anal yzing the Rows over multielement airfoils on chimera overlaid grid systems.