1 |
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Identification of Impact Force and Location Using Distributed Sensors
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Choi, K
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American Institute of Aeronautics and Astronautics
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1996
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2 |
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Illustration of the Inclusion of Sound-Flow Interactions in Lighthill's Equation (TN)/
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Bogey, C
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American Institute of Aeronautics and Astronautics
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2003
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3 |
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Images of Dissipation Layers to Quantify Mixing Within a Turbulent Jet
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Feikema, D. A
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American Institute of Aeronautics and Astronautics
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1996
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4 |
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Impact of Axial Vortices on Mixing at a High Convective Mach Number (TN)/
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Parent, B
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American Institute of Aeronautics and Astronautics
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1900
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5 |
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Impact of Tab Location Relative to the Nozzle Exit Jet Distortion (TN)
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Reeder, M. F
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American Institute of Aeronautics and Astronautics
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1996
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6 |
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Implementation of an Adaptive Piezoelectric Sensoriactuator
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Vipperman, J. 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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Implicit Computation of Three-Dimensional Compressible Navier-Stokes Equations Using k-�Closure
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Gerolymos, G. A
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American Institute of Aeronautics and Astronautics
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1996
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8 |
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Implicit High-Order Compact Algorithm for Computational Acoustics
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Fung, K.-Y
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American Institute of Aeronautics and Astronautics
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1996
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9 |
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Implicit Method for Incompressible Flow Calculations in Three-Dimensional Ducts and Cascades
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Politis, E. S
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American Institute of Aeronautics and Astronautics
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1997
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10 |
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Implicit Solution Method for Incompressible Navier-Stokes Equations Including Two-Layer k-tau Turbulence Model
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Kueffer, J
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American Institute of Aeronautics and Astronautics
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1996
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11 |
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Implicit Technique for Three-Dimensional Turbulent Magnetoaerodynamics/
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Gaitonde, D. V
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American Institute of Aeronautics and Astronautics
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2003
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12 |
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Implicit Time-Stepping Methods for the Navier-Stokes Equations
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Badcock, K. 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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Implicit Upwind Residual-Distribution Euler and Navier-Stokes Solver on Unstructured Meshes
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Issman, E
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American Institute of Aeronautics and Astronautics
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1996
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14 |
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Importance of Instability in Impact Response and Damage Resistance of Composite Shells
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Wardle, B. L
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American Institute of Aeronautics and Astronautics
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1997
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15 |
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Improved Damage Location Accuracy Using Strain Energy-Based Mode Selection Criteria
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Doebling, S. W
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American Institute of Aeronautics and Astronautics
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1997
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16 |
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Improved Jet Coverage Through Vortex Cancellation
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Haven, B. A
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American Institute of Aeronautics and Astronautics
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1996
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17 |
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Improved Method for Determining Free-Free Modes Using Constrained Test Data (TN)
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Han, W.-Z
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American Institute of Aeronautics and Astronautics
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1997
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18 |
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Improved Mindlin Plate Stress Analysis for Laminated Composites in Finite Element Method
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Cho, M
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American Institute of Aeronautics and Astronautics
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1997
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19 |
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Improved Theory for Contact Indentation of Sandwich Panels
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Olsson, R
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American Institute of Aeronautics and Astronautics
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1996
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20 |
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Improved Transient Response Approximation for General Damped Systems
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Sepulveda, A. E
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American Institute of Aeronautics and Astronautics
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1996
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