scholarly journals Comparison of two methods of laminar-turbulent transition prediction for transonic speeds

2018 ◽  
Author(s):  
A. Sidorenko ◽  
S. Kirilovskiy ◽  
A. Boiko ◽  
K. Demyanko ◽  
Yu. Nechepurenko
Keyword(s):  
Transition Prediction ◽  
Turbulent Transition ◽  
Laminar Turbulent Transition

scholarly journals On the development of methods of the laminar-turbulent transition prediction

2021 ◽  
Author(s):  
A. V. Boiko ◽  
K. V. Demianko ◽  
A. V. Ivanov ◽  
S. V. Kirilovsiy ◽  
D. A. Mischenko ◽  
...  
Keyword(s):  
Transition Prediction ◽  
Turbulent Transition ◽  
Laminar Turbulent Transition

Laminar-Turbulent Transition Prediction on Industrial CFD Applications

2022 ◽  
Author(s):  
Krishna Zore ◽  
Alexey Matyushenko ◽  
Shoaib Shah ◽  
Cristhian Aliaga ◽  
John Stokes ◽  
...  
Keyword(s):  
Transition Prediction ◽  
Turbulent Transition ◽  
Cfd Applications ◽  
Laminar Turbulent Transition

scholarly journals Database Approach for Laminar-Turbulent Transition Prediction: Navier–Stokes Compatible Reformulation

AIAA Journal ◽  
2017 ◽  
Vol 55 (11) ◽  
pp. 3648-3660 ◽  
Author(s):  
Guillaume Bégou ◽  
Hugues Deniau ◽  
Olivier Vermeersch ◽  
Grégoire Casalis
Keyword(s):  
Navier Stokes ◽  
Transition Prediction ◽  
Turbulent Transition ◽  
Laminar Turbulent Transition

scholarly journals Database Approach for Laminar-Turbulent Transition Prediction on Heated Wall

2020 ◽  
Author(s):  
Julien Saint-James ◽  
Hugues Deniau ◽  
Olivier Vermeersch ◽  
Estelle Piot
Keyword(s):  
Heated Wall ◽  
Transition Prediction ◽  
Turbulent Transition ◽  
Laminar Turbulent Transition

Aerodynamic Optimization of an Impulse Turbine Cascade Including Laminar/Turbulent Transition Prediction

2010 ◽  
Author(s):  
Ernesto Benini ◽  
Claudio Comis da Ronco ◽  
Rita Ponza
Keyword(s):  
Total Pressure ◽  
Pressure Coefficient ◽  
Optimization Procedure ◽  
Turbine Rotor ◽  
Aerodynamic Optimization ◽  
Impulse Turbine ◽  
Pressure Losses ◽  
Transition Prediction ◽  
Turbulent Transition ◽  
Laminar Turbulent Transition

Aerodynamic optimization of an impulse turbine rotor cascade is described in this paper. The aim of the optimization is to minimize the total pressure losses through the cascade by reshaping the turbine airfoil. For a more realistic calculation of the boundary layer and the associated losses, laminar/turbulent transition is computed by means of the commercial CFD code Fluent. The solver underwent an accurate validation before it is inserted into the optimization loop. A proper optimization procedure is developed which is based on a sequential use of two modules: first, a global search is performed using a genetic algorithm, then a local optimization is carried out by means of a Sequential Quadratic Programming (SQP) algorithm. The benefits of this approach are demonstrated, in that the total pressure coefficient of the cascade can be lowered up to 25%.

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