Detalles de la Emisión
Detalles de la Emisión

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Título Vol. 37 No. 2 (Feb. 1999)Emisión de Seriada
Parte de AIAA Journal
Publicación American Institute of Aerodynamics and Astronautics, Febrero 1999
Descripción Física 145-288p.
Idioma Inglés;
Materia(s) Publicaciones seriadas; INGENIERA AERONAUTICA; Publicaciones científicas; Dinámica de fluídos;
Nota(s) Jet Mixing Noise from Fine-Scale Turbulence, p.145; Noise Measurement in Supersonic Jets Treated with the Mach Wave elimination method, p.154; Calculation of Basic sound Radiation of Axisymmetric Jets by Direct Numerical simulations, p.161; Multiblock Approach for Calculating Incompressible Fluid Flows on Unstructured Grids, p.168; finite volume Discretization aspects for Viscous flows on Mixed Unstructured Grids, p.177; Airfoil design on Unstructured Grids for turbulent Flows, p.185; Near Exit Plane Effects Caused by Primary and Primary-Plus-Secondary Tabs, p.192; Three-Dimensional Temporal Instability of Compressible Gas Jets Injected in Liquids, p.202; Chemical Kinetics and Self Ignition in a Model Supersonic Hydrogen-Air Combustor, p.208; Molecular Dynamics Simulation of Piston-Driven Shock Wave in Hard Sphere Gas, p.215; Perturbation Technique for non-self-Adjoint System with Repeated Eigenvalues, p.222; Failure of Sandwich to Laminate Tapered Composite structures, p.227; Response of composite shells with Cutouts to international Pressure and Compression Loads, p.232; Thermoviscoelastic Analysis of Composite Structures Using a Triangular Flat Shell Element, p.238; Dynamics of Delaminated composite Plates with Piezoelectric Actuators, p.248; Use of Fracture Mechanics and Shape Optimization for Component Designs, p255; Using the two-Branch Tournament Genetic Algorithm for Multiobjetive Design, p.261; Prediction of Developing Turbulent Pipe Flow by a Modified K-E-y Model, p.268; Sound Amplification by a Supersonic Jet, p.270; Numerical Stability Conditions in the Calculation of Potential Velocity Fields, p.272; Experimental Buckling of thin composite Cylinders in compression, p.276; Forward Flight Effects on Counterflow Thrust Vector Control of a supersonic Jet, p.279; Streamwise Vortices in the Outer Layer of Wall jets with convex Curvature, p.281; Two-Layer Approach combining Reynolds Stress and Low-Reynolds-Number K-E Models, p.283.
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0000079789Universidad de San Buenaventura - Sede BogotáColección Depósito AI/JO 1999 No. 2DisponibleHemerotecaSolicitar