1 |
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Sandwich-Plate Vibration Analysis: Three-Layer Quasi-Three-Dimensional Finite Element Model/
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Nabarrete, A
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American Institute of Aeronautics and Astronautics
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2003
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2 |
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Scalar Transport in a Swirling Transverse Jet
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Niederhaus, C. E
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American Institute of Aeronautics and Astronautics
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1997
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3 |
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Scaling Laws of Cylindrical Shells Under Lateral Pressure (TN)
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Tabiei, A
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American Institute of Aeronautics and Astronautics
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1997
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4 |
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Scaling of Icing Tests: A Review of Recent Progress/
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Kind, R. J
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American Institute of Aeronautics and Astronautics
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2003
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5 |
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Scaling of the Bursting Frequency for Turbulent Boundary Layers Approaching Separation (TN)
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Tillman, T. G
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American Institute of Aeronautics and Astronautics
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1996
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6 |
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Scanned- and Fixed-Wavelength Absorption Diagnostics for Combustion Measurements Using Multiplexed Diode Lasers
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Baer, D. S
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American Institute of Aeronautics and Astronautics
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1996
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7 |
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Second-Order Small-Disturbance Solution for Wing at Supersonic Speeds
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Luo, S
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American Institute of Aeronautics and Astronautics
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1996
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8 |
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Sectional Flow Structures in Near Wake of Elevated Jets in a Crossflow/
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Huang, R. F
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American Institute of Aeronautics and Astronautics
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2003
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9 |
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Selective Modal Transducers for Anisotropic Rectangular Plates: Experimental Validation
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Miller, S. E
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American Institute of Aeronautics and Astronautics
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1997
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10 |
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Self-Contained Automated Methodology for Optimal Flow Control
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Joslin, R. D
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American Institute of Aeronautics and Astronautics
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1997
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11 |
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Self-Similar Viscous Incompressible Flow Along an Unbounded Corner
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Vasiliev, V. I
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American Institute of Aeronautics and Astronautics
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1996
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12 |
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Semiactive Vibration Suppression by Variable-Damping Members
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Onoda, J
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American Institute of Aeronautics and Astronautics
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1996
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13 |
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Semiactive Vibration Suppression with Electrorheological-Fluid Dampers
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Onoda, J
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American Institute of Aeronautics and Astronautics
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1997
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14 |
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Semianalytical Differential Quadrature Solution for Free Vibration Analysis of Rectangular Plates
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Bert, C. W
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American Institute of Aeronautics and Astronautics
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1996
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15 |
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Sensitivity Analysis of the Aeroacoustic Response of Turbomachinery Blade Rows
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Lorence, C. B
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American Institute of Aeronautics and Astronautics
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1996
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16 |
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Sensitivity to the Smagorinsky Constant in Turbulent Jet Simulations (TN)/
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Uzun, A
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American Institute of Aeronautics and Astronautics
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2003
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17 |
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Sensor Placement and Structural Damage Identification from Minimal Sensor Information
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Cobb, R. G
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American Institute of Aeronautics and Astronautics
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1997
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18 |
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Shape and Placement of Piezoelectric Sensors for Panel Fluter Limit-Cycle Suppression
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Lai, Z
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American Institute of Aeronautics and Astronautics
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1996
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19 |
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Shape Control of Vibrating Simply Supported Rectangular Plates
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Batra, R. C
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American Institute of Aeronautics and Astronautics
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1996
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20 |
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Shape Optimization with Buckling and Stress Constraints (TN)
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Botkin, M. E
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American Institute of Aeronautics and Astronautics
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1996
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