| 81 |
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INTERDISCIPLINARY TOPICS - Recent Advances in Detonation Techniques for High-Enthalpy Facilities/
|
Lu, F K
|
American Institute of Aeronautics and Astronautics
|
2000
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| 82 |
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INTERDISCIPLINARY TOPICS - Required Relationship Between Objective Function and Pareto Frontier Orders: Practical Implications/
|
Messac, A
|
American Institute of Aeronautics and Astronautics
|
2001
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|
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| 83 |
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INTERDISCIPLINARY TOPICS - Survey of Shape Parameterization Techniques for High-Fidelity Multidisciplinary Shape Optimization/
|
Samareh, J A
|
American Institute of Aeronautics and Astronautics
|
2001
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| 84 |
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INTERDISCIPLINARY TOPICS - Temperature- and Pressure-Sensitive Paint Measurements in Short-Duration Hypersonic Flow/
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Hubner, J P
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American Institute of Aeronautics and Astronautics
|
2001
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| 85 |
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INTERDISCIPLINARY TOPICS - Temperature Measurements in a Hypersonic Boundary Layer Using Planar Laser-induced Fluorescence (TN)/
|
Palma, P C
|
American Institute of Aeronautics and Astronautics
|
2000
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| 86 |
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INTERDISCIPLINARY TOPICS - Time Response of Anodized Aluminum Pressure-Sensitive Paint/
|
Sakaue, H
|
American Institute of Aeronautics and Astronautics
|
2001
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| 87 |
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INTERDISCIPLINARY TOPICS - Two-Color Planar Doppler Velocimetry/
|
Arnette, S A
|
American Institute of Aeronautics and Astronautics
|
2000
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| 88 |
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Interface Wavelength Between Supersonic Jets and Subsonic Flowfields
|
De Chant, L. J
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American Institute of Aeronautics and Astronautics
|
1996
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|
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| 89 |
|
Interference Between a Cylindrical Bow Shock and a Plane Oblique Shock
|
Borovoy, V. Y
|
American Institute of Aeronautics and Astronautics
|
1997
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|
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| 90 |
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Intergrid-Boundary Definition Method for Overact Unstructured Grid Approach/
|
Nakahashi, K
|
American Institute of Aeronautics and Astronautics
|
2000
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| 91 |
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Intrinsic Equations for the Nonlinear Dynamics of Space Beams
|
Libai, A
|
American Institute of Aeronautics and Astronautics
|
1996
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| 92 |
|
Introduction to Aerodynamic Measurement Technology Special Section
|
Pitz, R. W
|
American Institute of Aeronautics and Astronautics
|
1996
|
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| 93 |
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Inverse Aeroacoustic Problem for a Streamlined Body Part 1: Basic Formulation
|
Grace, S. P
|
American Institute of Aeronautics and Astronautics
|
1996
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| 94 |
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Inverse Aeroacoustic Problem for a Streamlined Body Part 2: Accuracy of Solutions
|
Grace, S. P
|
American Institute of Aeronautics and Astronautics
|
1996
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| 95 |
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Inverse and Direct Airfoil Design Using a Multiobjective Genetic Algorithm
|
Vicini, A
|
American Institute of Aeronautics and Astronautics
|
1997
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| 96 |
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Inverse-Imaging Method for Detection of a Vortex in a Channel/
|
Suzuki, T
|
American Institute of Aeronautics and Astronautics
|
2003
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|
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| 97 |
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Inverse Method for Identification of Acoustic Sources at Launch Vehicle Liftoff/
|
Alestra, S
|
American Institute of Aeronautics and Astronautics
|
2003
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| 98 |
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Investigation of Factors Affecting lced-Airfoil Aerodynamics/
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Lee, S
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American Institute of Aeronautics and Astronautics
|
2003
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| 99 |
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Investigation of High-Order Upwinded Differencing for Vortex Convection
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Wake, B. E
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American Institute of Aeronautics and Astronautics
|
1996
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| 100 |
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Investigation of Large-Scale Structures in Supersonic Planar Base Flows
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Smith, K. M
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American Institute of Aeronautics and Astronautics
|
1996
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