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A Gradient-based Optimization Method for Natural Laminar Flow Design : OPTLAM Project Final Report

A Gradient-based Optimization Method for Natural Laminar Flow Design : OPTLAM Project Final Report

Ardeshir Hanifi | Jan O. Pralits | Olivier Amoignon | David Tempelmann | J. Pralits | O. Amoignon | A. Hanifi | David Tempelmann

[1] D. Henningson,et al. Shape Optimization for Delay of Laminar-Turbulent Transition , 2006 .

[2] Richard L. Campbell,et al. Method for the Constrained Design of Natural Laminar Flow Airfoils , 1997 .

[3] Jan O. Pralits,et al. Optimization of steady suction for disturbance control on infinite swept wings , 2003 .

[4] E. Bradford,et al. A Method for the Constrained Design of Natural Laminar Flow Airfoils , 1996 .

[5] Marian Nemec,et al. Towards efficient aerodynamic shape optimization based on the Navier-Stokes equations , 2001 .

[6] Ilan Kroo,et al. Multidisciplinary optimization of a natural laminar flow supersonic aircraft , 1999 .

[7] P. Spalart,et al. Linear and nonlinear stability of the Blasius boundary layer , 1992, Journal of Fluid Mechanics.

[8] O. Amoignon. AESOP—a numerical platform for aerodynamic shape optimization , 2010 .

[9] A. Jameson. Optimum aerodynamic design using CFD and control theory , 1995 .

[10] M. Berggren,et al. Adjoint of a median-dual finite-volume scheme : Application to transonic aerodynamic shape optimization , 2006 .

[11] D. Quagliarella,et al. Natural Laminar Flow Design of a Supersonic Transport Jet Wing Body , 2009 .

[12] J. V. Ingen. A suggested semi-empirical method for the calculation of the boundary layer transition region , 1956 .