Advanced Engineering Dynamics Solutions Paperback – 27 October 1995 by Jerry H. Ginsberg (Author) See all formats and editions Hide other formats and editions. Price New from Used from Paperback, 27 October 1995 'Please retry' — — — Paperback — Product details.
Module Lead: Professor Lin Ma | Profile | Email Other Teaching Staff: Professor Ning Qin | Profile | Email QAA Framework Credit Level: 7 | Credits: 15 Semester: Autumn Pre-Requisites: MEC208 or AER298, or equivalent in the case of the MSc Co-Requisites: None Restrictions: None |
Engineering Dynamics Pdf
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Engineering Dynamics Book
Module Overview | Module DescriptionThe module introduces advanced subjects in fluid mechanics and focuses on the theory and applications of the fundamental physical laws governing Newtonian and non-Newtonian fluid flows. The Navier-Stokes and continuity equations are revisited and the Energy and the general Transport Equations for fluid flows will be derived. A key skill developed is problem solving in the area of advanced fluid mechanics through how equations, boundary conditions and computational models may be adapted and simplified to describe a wide variety of engineering flows such as creeping, laminar, turbulent, incompressible and compressible flows. Module Syllabus1. Introduction • Basic concepts of fluid dynamics • Kinematics of fluid flows: translation/deformation/rotation, strain rates (tensor), stress, vorticity (tensor), etc. • Revision on vector/tensor notations. 2. Method of flow analysis • Frame of references: Lagrange/Eulerian, stream functions, • Revision on N-S Equations • Transport Equation for fluid flows. 3. Analytical Solutions for Simple Fluid Flows • Stokes flow • Potential flow 4. Boundary Layer Flow - The concept and theory • Derivation of Boundary layer equations • The Blasius solutions for flow over a flat plate • Displacement Thickness, Momentum Thickness, The Integral Method 5. Boundary Layer Flow - Separation, Transition and Turbulent BL • Boundary layer flow transition and separation • Turbulent BL, Structure and velocity profiles, stress distribution/wall friction 6. Compressible flows - Basic • Speed of sound and derivation of the Mach number • Classification of speed range for compressible flows: from subsonic to hypersonic • Revisit isentropic relations 7. Compressible flows – inviscid • Revisit of normal shock relations • Oblique shock waves and analytical relations • Transonic, supersonic and hypersonic flows 8. Compressible flows - viscous • Compressible flow boundary layer: temperature profiles in the boundary layer • Shock boundary layer interaction • Control of SBLI 9. Transonic aerodynamics and drag reduction • Composition of aircraft drag • Drag rise Mach number and supercritical aerofoils • Swept wing • Shock control for transonic wings 10. Supersonic and hypersonic aerodynamics • Delta wing and supersonic aircraft • Sonic boom and its reduction for SST • Spikes for hypersonic drag and heating reduction 11. Revision | ||||||||||||||||||
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