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Kim, Sangho - Department of Aeronautics and Astronautics, Stanford University
Development Introducing
Reduction of the Adjoint Gradient Formula in the Continuous Limit Antony Jameson
Design Optimization of MultiElement Aerodynamic Configurations Using a Viscous
Sonic Boom Reduction using an Adjoint Method for Supersonic Transport Aircraft
DESIGN OPTIMIZATION OF HIGH-LIFT CONFIGURATIONS USING A VISCOUS ADJOINT-BASED METHOD
A GRADIENT ACCURACY STUDY FOR THE ADJOINT-BASED NAVIER-STOKES DESIGN METHOD
Integrated Simulations for Multi-Component Analysis of Gas Turbines : RANS Boundary Conditions
AIAA 20004741 Two-dimensional High-Lift
A Gradient Accuracy Study for the Adjoint-Based Navier-Stokes Design Method
Design Optimization of MultiElement HighLift Configurations Using a Viscous Continuous Adjoint Method
