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Showing results 1 to 10 of 10

Issue Date	Title / Author(s) / Citation	File	Altmetrics
2007-03	Automated Design Methodology of Turbulent Internal Flow using Discrete Adjoint Formulation Lee, Byung Joon; Kim, Chongam Aerospace Science and Technology 11 (2007) 163-173	DOI
2007-05	Aerodynamic Shape Optimization using Discrete Adjoint Formulation based on Overset Mesh Technique Lee, Byung Joon; Yim, Jin Woo; Yi, Jun Sok; Kim, Chongam KSAS International Journal, v.8, no.1, pp.95-104	view file link
2008-09	Aerodynamic Redesign Using Discrete Adjoint Approach on Overset Mesh System Lee, Byung Joon; Kim, Chongam Journal of Aircraft Vol.45, No.5, pp. 1643-1653	DOI
2008-09	Aerodynamic redesign using discrete adjoint approach on overset mesh system Lee, Byung Joon; Kim, Chongam Journal of Aircraft, Vol.45 No.5, pp.1643-1653	DOI
2010-09	Optimizing a Boundary-Layer-Ingestion Offset Inlet by Discrete Adjoint Approach Lee, Byung Joon; Liou, Mena-Sing; Kim, Chongam AIAA JOURNAL Vol.48 No.9, pp. 2008-2016	DOI
2010-09	Optimizing a Boundary-Layer-Ingestion Offset Inlet by Discrete Adjoint Approach Lee, Byung Joon; Liou, Mena-Sing; Kim, Chongam AIAA Journal, Vol.48 No.9, pp.2008-2016	DOI
2012-09	Exploring multi-stage shape optimization strategy of multi-body geometries using Kriging-based model and adjoint method Yim, JinWoo; Lee, Byung Joon; Kim, Chongam COMPUTERS & FLUIDS Vol.68, pp. 71-87	DOI
2012-09	Exploring multi-stage shape optimization strategy of multi-body geometries using Kriging-based model and adjoint method Yim, JinWoo; Lee, Byung Joon; Kim, Chongam Computers and Fluids, Vol.68, pp.71-87	DOI
2012-11	Adjoint-Based Design Optimization of Vortex Generator in an S-Shaped Subsonic Inlet Yi, JunSok; Kim, Chongam; Lee, Byung Joon AIAA JOURNAL Vol.50 No.11, pp. 2492-2507	DOI
2012-11	Adjoint-Based Design Optimization of Vortex Generator in an S-Shaped Subsonic Inlet Yi, JunSok; Kim, Chongam; Lee, Byung Joon AIAA Journal, Vol.50 No.11, pp.2492-2507	DOI

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