| 1 |
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Accelerated Iterative Procedure for Calculating Eigenvector Derivatives
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Zhang, O
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American Institute of Aeronautics and Astronautics
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1997
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| 2 |
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Active Control of Panel Oscillation Induced by Accelerating Boundary Layer and Sound
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Maestrello, L
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American Institute of Aeronautics and Astronautics
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1997
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| 3 |
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Adaptive Finite Volume Upwind Approaches for Aeroacoustic Computations
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Hwang, C. J
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American Institute of Aeronautics and Astronautics
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1997
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| 4 |
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Adaptive Monte Carlo Simulation for Time-Variant Reliability Analysis ofBrittle Structures
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Mahadevan, S
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American Institute of Aeronautics and Astronautics
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1997
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| 5 |
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Adaptive Remeshing for the k-�Model of Turbulence
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Pelletier, D
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American Institute of Aeronautics and Astronautics
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1997
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| 6 |
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Adaptive Topology Optimization of Shell Structures
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Maute, K
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American Institute of Aeronautics and Astronautics
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1997
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| 7 |
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Aeroacoustic Boundary Element Method Using Analytical/Numerical Matching
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Epstein, R. J
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American Institute of Aeronautics and Astronautics
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1997
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| 8 |
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Aerodynamically Accurate Three-Dimensional Navier-Stokes Method (TN)
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Epstein, B
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American Institute of Aeronautics and Astronautics
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1997
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| 9 |
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Aeroelastic Sensitivity Analysis of Wings Using Automatic Differentiation
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Isaac, J. C
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American Institute of Aeronautics and Astronautics
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1997
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| 10 |
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Airfoil Boundary-Layer Development and Transition with Large Leading-Edge Roughness
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Kerho, M. F
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American Institute of Aeronautics and Astronautics
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1997
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| 11 |
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Algebraic Turbulence Modeling for Swept Shock-Wave/Turbulent Boundary-Layer Interactions
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Panaras, A. G
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American Institute of Aeronautics and Astronautics
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1997
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| 12 |
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Analysis of Streamline Curvature Effects on Wall-Bounded Turbulent Flows
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Luo, J
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American Institute of Aeronautics and Astronautics
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1997
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| 13 |
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Analysis of Uncertain Structural Systems Using Interval Analysis
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Rao, S. S
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American Institute of Aeronautics and Astronautics
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1997
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| 14 |
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Analytical Study of the Oblique Reflection of Detonation Waves
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American Institute of Aeronautics and Astronautics
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1997
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| 15 |
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Application of Chimera/Unstructured Hybrid Grids for Conjugate Heat Transfer
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Kao, K.-H
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American Institute of Aeronautics and Astronautics
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1997
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| 16 |
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Application of Nonlinear Localization to the Optimization of a VibrationIsolation System
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Nayfeh, T. A
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American Institute of Aeronautics and Astronautics
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1997
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| 17 |
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Approximating Collisional Freestream Attenuation at Transitional KnudsenNumbers
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King, L. B
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American Institute of Aeronautics and Astronautics
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1997
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| 18 |
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Approximation of System Reliabilities Using a Shooting Monte Carlo Approach
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Brown, S. A
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American Institute of Aeronautics and Astronautics
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1997
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| 19 |
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Attenuation of Shock Waves in Gas-Particle Mixtures
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Das, H. K
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American Institute of Aeronautics and Astronautics
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1997
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| 20 |
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Automatic Control of Laminar Boundary-Layer Transition
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Nelson, P. A
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American Institute of Aeronautics and Astronautics
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1997
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