Detalles de la Emisión
Detalles de la Emisión

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Título Vol. 37 No. 11 (Nov. 1999)Emisión de Seriada
Parte de AIAA Journal
Publicación American Institute of Aerodynamics and Astronautics, Noviembre 1999
Descripción Física 1337-1527p.
Idioma Inglés;
Materia(s) Publicaciones seriadas; Ingeniería Aeronáutica; Investigación y Desarrollo; TECNOLOGÍA AERONÁUTICA; MATERIALES AERONÁUTICOS;
Nota(s) Avionics: A “New” Senior Partner in Aeronautics, p.1337; Limit Cycle Oscillations of Delta Wing Models in low subsonic flow, p.1355; Measurements of Supersonic Helium/Air Mixture Jets, p.1363; Effect of Isolated Micron-Sized Roughness on Transition in Swept Wing flows, p. 1370; Steady and Unsteady flow simulations Using the Hybrid flow Solver AVBP, p.1378; Numerical Simulation of Dynamic Stall Using am Improved Advection Upwind Splitting Method, p.1386; Aerodynamic Influence coefficient Computation on Parallel Using Euler/Navier-Stokes Equations on Parallel Computers, p.1393; Large Eddy Simulation of Rearward-Facing Step flow, p.1401; Aerodynamic Design Optimization on Unstructured Meshes Using the Navier-Stokes Equations, p.1411; Simulation of Reacting Droplets Dispersed in Isotropic Turbulence, p.1420; Theory of Flame Histories in Droplet Combustion at Small Stoichiometric Fuel-Air Ratios, p.1426; Conditional Analysis of Wall Pressure Fluctuations in Plume-Induced Separated Flowfields, p.1436; Extraction of Substructural flexibility from Global Frequencies and mode Shapes, p.1444; Rates of Change of Eigenvalues and Eigenvectors in Damped Dynamic System, p.1452; Distributed Piezoelectric Method for vibration control of smart Plates, p.1459; Analytical solution for Rectangular Thick Laminated Plated Subjected to Arbitrary Boundary Conditions, p.1464; Nonlinear Behavior of Sandwich Panels with a Transversely flexible Core, p.1474; Bidirectional evolutionary Method for Stiffness Optimization, p.1483; Nonlinear Dynamic finite Element Analysis of composite Cylindrical Shells Considering Large Rotations, p.1489; Basic Development of Hybrid finite element Method for Midfrequency Structural Vibrations, p.1495; Structural Redesign for forced response with Proportional Damping by Large Admissible Perturbations, p.1506; Structural Optimization with Static Aeroelastic and Stress Constraints Using Expandable Modal Basis, p.1514.
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0000079797Universidad de San Buenaventura - Sede BogotáColección Depósito Ai/Jo 1999 No.11DisponibleHemerotecaSolicitar