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Description
(Text)
This book describes an engineering approach based on interactive boundary-layer and stability-transition theories, both developed by the author, for calculating aerodynamic flows. This is the first time these powerful computational techniques have been published in book form.
(Table of content)
Interactive Boundary-Layer Approach for Airfoils.- Two-Dimensional Incompressible Flows: Inviscid Method.- Two-Dimensional Incompressible Flows: Boundary-Layer Method.- Two-Dimensional Incompressible Flows: Inviscid Method.- Applications of the Calculation Method: Airfoils in Incompressible Flows.- Two-Dimensional Compressible Flows.- Two-Dimensional Incompressible Unsteady Flows: Inviscid Method.- Two-Dimensional Unsteady Incompressible Flows: Boundary-Layer Method.- Application of the Calculation Method: Airfoils in Incompressible Unsteady Flow.- Three-Dimensional Incompressible Flows: Inviscid Method.- Three-Dimensional Flows: Boundary-Layer Method.- Three-Dimensional Flows: Transition Method.- Applications of the Calculation Method to Three-Dimensional Subsonic and Transonic Flows.



