| 1 |
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A Mechanism for Flame Acceleration in Narrow Tubes (TN)/
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Ott, J. D
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American Institute of Aeronautics and Astronautics
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1900
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| 2 |
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A Mixing Theory for the Interaction Between Dissipative Flows and Nearly Isentropic Streams/
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Crocco, L
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American Institute of Aeronautics and Astronautics
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1900
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| 3 |
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Mach Wave Elimination in Supersonic Jets
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Papamoschou, D
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American Institute of Aeronautics and Astronautics
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1997
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| 4 |
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Mass Spectrometer Measurement of Test Gas Composition in a Shock Tunnel (TN)
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Skinner, K. A
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American Institute of Aeronautics and Astronautics
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1996
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| 5 |
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Matching Inviscid/Boundary-Layer Flowfields
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DeJarnette, F. R
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American Institute of Aeronautics and Astronautics
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1996
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| 6 |
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Maysel's Formula Generalized for Piezoelectric Vibrations: Application to Thin Shells of Revolution
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Irschik, H
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American Institute of Aeronautics and Astronautics
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1996
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| 7 |
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Mean and Turbulence Measurements in the Near Field of a Wingtip Vortex
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Chow, J. S
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American Institute of Aeronautics and Astronautics
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1997
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| 8 |
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Mean Flowfield Scaling of Supersonic Shock-Free Three-Dimensional Turbulent Boundary Layer/
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Konrad, W
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American Institute of Aeronautics and Astronautics
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2000
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| 9 |
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Mean Velocity and Static Pressure Distributions of a Circular Jet (TN)
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Islam, M. T
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American Institute of Aeronautics and Astronautics
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1997
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| 10 |
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Measurements in Rollup Region of the Tip Vortex from a Rectangular Wing
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Ramaprian, B. R
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American Institute of Aeronautics and Astronautics
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1997
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| 11 |
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Measurements of the Triple Shock Wave/Turbulent Boundary-Layer Interaction
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Garrison, T. J
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American Institute of Aeronautics and Astronautics
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1996
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| 12 |
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Measurements of the Velocity and Turbulence Structure of a Rotor Tip Vortex
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Han, Y. O
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American Institute of Aeronautics and Astronautics
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1997
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| 13 |
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Measurements of Velocity and Vorticity Fields Around a Pitching Swept Wing (TN)
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Rymarz, P. B
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American Institute of Aeronautics and Astronautics
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1997
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| 14 |
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Method for Structural Model Update Using Dynamically Measured Static Flexibility Matrices
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Denoyer, K. K
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American Institute of Aeronautics and Astronautics
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1997
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| 15 |
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Methods for Calculating the Subsonic Aerodynamic Center of Finite Wings/
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Rodden, W. P
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American Institute of Aeronautics and Astronautics
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2003
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| 16 |
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Methods for Predicting Phenomena in the High-Speed Flow of Gases/
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Lighthill, M. J
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American Institute of Aeronautics and Astronautics
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1900
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| 17 |
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Methods for Visualizing Hypersonic Shock-Wave/Boundary-Layer InteractionUsing Electrical Discharges
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Nishio, M
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American Institute of Aeronautics and Astronautics
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1996
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| 18 |
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Micromechanical Analyses of Instabilities in Braided Glass Textile Composites/
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Quek, S. C
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American Institute of Aeronautics and Astronautics
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2003
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| 19 |
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Micromechanics-Based Modeling of Woven Polymer Matrix Composites/
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Bednarcyk, B. A
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American Institute of Aeronautics and Astronautics
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2003
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| 20 |
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Micromechanics of Composites with Shape Memory Alloy Fibers in Uniform Thermal Fields
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Birman, V
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American Institute of Aeronautics and Astronautics
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1996
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