Transition Location Effect on Shock Wave Boundary Layer Interaction كتب أخرى بهذه السلسلة

Fundamentals of High Lift for Future Civil Aircraft

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Future Space-Transport-System Components under High Thermal and Mechanical Loads

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Advances in Critical Flow Dynamics Involving Moving/Deformable Structures with Design Applications

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Turbulence and Interactions

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Noise and Vibration Mitigation for Rail Transportation Systems

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New Results in Numerical and Experimental Fluid Mechanics XIII

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Active Flow and Combustion Control 2021

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Smart Morphing and Sensing for Aeronautical Configurations

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New Results in Numerical and Experimental Fluid Mechanics XIV

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Towards Effective Flow Control and Mitigation of Shock Effects in Aeronautical Applications

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Advanced Aircraft Understanding via the Virtual Aircraft Model

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Computational Science and High Performance Computing

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Advances in High Performance Computing and Computational Sciences

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FLOMANIA - A European Initiative on Flow Physics Modelling

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MEGAFLOW - Numerical Flow Simulation for Aircraft Design

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