Extension to Turbulent Flow and Numerical Verification for Aerodynamic Optimization Design Method Based on Discrete Adjoint Theory[J]. 2013, 47(1): 37-42.
DOI:
Extension to Turbulent Flow and Numerical Verification for Aerodynamic Optimization Design Method Based on Discrete Adjoint Theory[J]. 2013, 47(1): 37-42.DOI: 10.7652/xjtuxb201301008.
Extension to Turbulent Flow and Numerical Verification for Aerodynamic Optimization Design Method Based on Discrete Adjoint Theory
The aerodynamic optimization design method was extended to turbulent flow environment
and a discrete adjoint solver applicable to the turbulent flow environment was implemented. On the basis of the solver
an aerodynamic optimization design platform was established by coupling the parameterization technology
grid generation technology
an in-house flow solver
the discrete adjoint solver and optimization technology. A typical transonic two-dimensional cascade was optimized based on the platform with the entropy generation being taken as the optimization function. Moreover
a mass flow ratio constraint was added to the objective function by using the penalty function method to keep the mass flow ratio constant. The optimization results show that the entropy generation of the optimized cascade decreases by 17.7% compared with that of the baseline cascade
demonstrating the correctness and effectiveness of the discrete adjoint solver developed.
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references
PIRONNEAU O. On optimum shapes in Stokes flow [J]. Journal of Fluid Mechanics, 1973, 59(2): 117-128.
JAMESON A. Aerodynamic design via control theory [J]. Journal of Scientific Computing, 1988, 3(3): 233-260.
ANDERSON W K, BONHAUS D L. Airfoil design on unstructured grids for turbulent flows [J]. AIAA Journal, 1999, 37(2): 185-191.
ZHANG Chaolei, LI Haitao, FENG Zhenping. Aerodynamic optimization design of turbomachinery cascade based on discrete adjoint method [J]. Journal of Engineering Thermophysics, 2012, 33(1): 47-50.
ZHANG Chaolei, FENG Zhenping. Aerodynamic shape design optimization for turbomachinery cascade based on discrete adjoint method, ASME Paper GT2011-45805 [R]. New York, NY, USA: ASME, 2011.
ZHANG Chaolei, LU Juan, FENG Zhenping. Inverse design of turbomachinery cascade based on discrete adjoint method [J]. Journal of Engineering Thermophysics, 2012, 33(4): 583-586.
BLAZEK J. Computational fluid dynamics: principles and applications [M]. Amsterdam, The Netherlands: Elsevier, 2001: 245-247.