Overview of the NASA Microgravity Combustion Program, p.1337; Structure and Soot Properties of Nonbuoyant Ethylene/Air Laminar Jet Diffusion Flames, p.1346; Experimental Study of Flame Balls in space: Preliminary Results from STS-83, p.1361; Microgravity n-Heptane Droplet Combustion in Oxygen Mixtures at Atmospheric Pressure, p.1369; Analytical comparison of the Acoustic Analogy and Kirchhoff Formulation for Moving Surfaces, p.1379; Broadband Self-Noise From a ducted Fan, p.1387; Influence of Nozzle geometric on the Noise of High-speed Jets, p.1396; K-E and Reynolds Stress Turbulence model comparisons for two-dimensional Injection Flows, p.1401, Essentially Nonoscillatory Euler Solutions on Unstructured Meshes Using Extrapolation, p.1413; Solution of the Euler Equations Using an Implicit Dual-Time Method, p.1417; Simulations of Planar Flapping Jets in Confined Channels, p.1425; Suppression off Flame Wrinkling by Buoyancy: The Baroclinic Stabilization Mechanism, p.1432; Large-Eddy Simulations and Lidar Measurements of Vortex-Pair Breakup in Aircraft Wakes, p.1439; Space-Based-Laser Wavelength Selection for Existing Beam Control Technology Levels, p.1446; Particle Image Velocimetry via Wavelet Analysis, p.1451; Luminescent Oil-Film Skin-Friction Meter, p.1460; Identification Approach to estimate Buckling Load of Damaged Composite Plates, p.1479; Transient Response Analysis of nonlinear Modally Coupled Structural Dynamics Equations of Motion, p.1486; Multiple-Criterion Method for Determining Structural Damage, p.1494; Dynamic Response of Initially Loaded Piezoelectric Plates Composed of Short Fibers, p.1502; Practical Procedures for Reliability Estimation of Spacecraft Structures and Their Components, p.1509; Pretwisted Nonuniform Beams with Time-Dependent elastic Boundary Conditions, p.1516; Three-Dimensional Free Vibration of Pretwisted Beams, p.1524; Elasticity Approach for Determination Buckling of Composite Beam Plates, p.1529.
