Abstract
The subject Computational Fluid Dynamics will be introduced with its applications to compute transonic inviscid and viscous flow past two- and three-dimensional bodies of practical interest in aerospace design and development. Development and implementation of vertex-based finite-volume methods for Euler and Navier–Stokes equations with an algebraic turbulence model will be discussed with some typical examples of aerospace applications, such as (i) Analysis of transonic flow past aerofoils including study of shock-induced separation at the foot of a strong shock, (ii) Analysis and design of aerofoils with flap configurations (GA(W)-2 and HANSA) including Gurney flaps, (iii) Internal flows through nozzles and cascades, (iv) Navier–Stokes analysis of round leading edge delta wing at high angles of attack and (v) Design and analysis of complete SARAS aircraft with sideslip will be presented.
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