Detalles de la Emisión
Detalles de la Emisión

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Título Vol. 38 No. 6 (Jun. 2000)Emisión de Seriada
Parte de AIAA Journal
Publicación American Institute of Aerodynamics and Astronautics, Junio 2000
Descripción Física 945-1110p.
Idioma Inglés;
Materia(s) Publicaciones seriadas; TECNOLOGÍA AERONÁUTICA; Dinámica de fluídos; Dinámica de fluídos - Modelos matemáticos; PROPULSIÓN DE AERONAVES; Propulsión; MATERIALES AERONÁUTICOS;
Nota(s) Modeling of Three-Dimensional Viscous Compressible Turbomachinery Flows Using Unstructured Hybrid Grids, p.945; Assessment and Modification of Two-Equation Turbulence Models, p.955; Control of Shock Loading from a Jet in a Flexible Structure`s Presence, p.972; Experimental Investigation of the Confluent Boundary Layer of a High-Lift System, p.978; Penetration and Spreading of Liquid Jets in an external-Internal Compression Inlet, p.989; Interwake Turbulence Properties of Homogeneous dilute Particle-Laden Flows, p. 995; Shock-Shape Alteration Caused by Interaction with Organized Structures, p.1002; Planar Doppler Velocimetry in a Large-Scale Facility, p.1010; Excitation of Thermoacoustic Instabilities by Interaction of Acoustics and Unstable Swirling flow, p.1025; Universal Perturbation Technique for Reanalysis of Non-Self-Adjoint Systems, p. 1035; Use of Substructural Transmission Zeros for Structural Health Monitoring, p.1040; Size Effects in Scaled Fiber Composites Under Four-Point Flexure Loading, p.1047; Thermo-Mechanical Response of Patched Plates, p.1055; Fusion of Wavelet Packets and Neural Network in Detection of Composites, p.1063; Dynamic Stability of a Free-Free Cylindrical Shell Under a Follover Force, p.1070; Dynamic Superelement Modeling Method for Compound Dynamic Systems, p.1078; Ability of Objective Functions to Generate Points on Nonconvex Pareto Frontiers, p.1084; Measurements in the Tip Vortex Roll-up Region of an Oscillating Wing (TN), 1092; Application of Acoustic Analogy to Automotive Engine-Cooling Fan Noise Prediction (TN), 1095; Navier-Stokes Prediction of internal flows with a three-Equation Turbulence Model (TN), p.1098; Model Vibration Analysis of Thick Laminated Composite Cylindrical Shells (TN), p1102; Review of Stiffness and Damping in mechanical Design, p.1108; Review of Advances in Turbulence VII, p.1109; Journal of the Japan society of Aeronautical and Space Sciences, p.1111.
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0000079803Universidad de San Buenaventura - Sede BogotáColección Depósito Ai/Jo 2000 No.6DisponibleHemeroteca