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Theses (Ph.D. / Sc.D._항공우주공학과)

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Design Optimization:2||6-DOF:1||Actuator Disk Method:1||Advanced Air Mobility:1||Aeroacoustics:1||Aerodynamic Design:1||Aerodynamic interaction:1||Aerodynamic interference:1||Aerodynamics:1||Aeroelastic Analysis:1||Aging analysis:1||Annual Energy Production (AEP):1||Aviation safety:1||Bending- Torsion Coupling:1||Blade Element Momentum Theory (BEMT):1||Cascade PID control:1||CFD:1||Chemical reaction kinetics:1||Classical Lamination Theory:1||Collision Avoidance:1||Combustion dynamics:1||Combustion instability:1||Composites:1||Conceptual Design:1||Convective heat transfer coefficient:1||convergence acceleration:1||Data-driven Approaches:1||Deadlock Resolution:1||deepreinforcementlearning:1||Defect-parametric reduced-order model:1||Design:1||Design Exploration:1||Design Parameters:1||Diffuser:1||Distributed Robot Systems:1||Distributedelectricpropulsion:1||Dual-nozzle gas turbine combustor:1||Dynamic inflow:1||Dynamic vortex tube:1||Electric Propulsion System:1||Electric Propulsion System Modeling:1||Electric Vertical Takeoff and Landing Aircraft:1||Energetic materials:1||Energy storage system:1||environmentallearning:1||extrinsic calibration:1||FEA:1||Finite Element Analysis(FEA):1||Flame-flame interaction:1||Flame-flow interaction:1

Issue Date	Title / Author(s) / Citation	File	Altmetrics
2021-02	Optimal Design of Wind Turbine Blade considering Multiple Variables using the Response Surface Method 이상래	view file link
2021-02	Structural responses due to the aero-acoustic pressure generated from a small-scale supersonic jet 주현식	view file link

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