| 1021 |
|
Low-Reynolds-Number Turbulent Flows in Locally Constricted Conduits: A Comparison Study/
|
Zhang, Z
|
American Institute of Aeronautics and Astronautics
|
2003
|
|
|
|
| 1022 |
|
LSENS: Multipurpose Kinetics and Sensitivity Analysis Code for Homogeneous Gas-Phase Reactions/
|
Radhakrishnan, K
|
American Institute of Aeronautics and Astronautics
|
2003
|
|
|
|
| 1023 |
|
Mach Wave Elimination in Supersonic Jets
|
Papamoschou, D
|
American Institute of Aeronautics and Astronautics
|
1997
|
|
|
|
| 1024 |
|
Mass Spectrometer Measurement of Test Gas Composition in a Shock Tunnel (TN)
|
Skinner, K. A
|
American Institute of Aeronautics and Astronautics
|
1996
|
|
|
|
| 1025 |
|
Matching Inviscid/Boundary-Layer Flowfields
|
DeJarnette, F. R
|
American Institute of Aeronautics and Astronautics
|
1996
|
|
|
|
| 1026 |
|
Maysel's Formula Generalized for Piezoelectric Vibrations: Application to Thin Shells of Revolution
|
Irschik, H
|
American Institute of Aeronautics and Astronautics
|
1996
|
|
|
|
| 1027 |
|
Mean and Turbulence Measurements in the Near Field of a Wingtip Vortex
|
Chow, J. S
|
American Institute of Aeronautics and Astronautics
|
1997
|
|
|
|
| 1028 |
|
Mean Flowfield Scaling of Supersonic Shock-Free Three-Dimensional Turbulent Boundary Layer/
|
Konrad, W
|
American Institute of Aeronautics and Astronautics
|
2000
|
|
|
|
| 1029 |
|
Mean Velocity and Static Pressure Distributions of a Circular Jet (TN)
|
Islam, M. T
|
American Institute of Aeronautics and Astronautics
|
1997
|
|
|
|
| 1030 |
|
Measurements in Rollup Region of the Tip Vortex from a Rectangular Wing
|
Ramaprian, B. R
|
American Institute of Aeronautics and Astronautics
|
1997
|
|
|
|
| 1031 |
|
Measurements of the Triple Shock Wave/Turbulent Boundary-Layer Interaction
|
Garrison, T. J
|
American Institute of Aeronautics and Astronautics
|
1996
|
|
|
|
| 1032 |
|
Measurements of the Velocity and Turbulence Structure of a Rotor Tip Vortex
|
Han, Y. O
|
American Institute of Aeronautics and Astronautics
|
1997
|
|
|
|
| 1033 |
|
Measurements of Velocity and Vorticity Fields Around a Pitching Swept Wing (TN)
|
Rymarz, P. B
|
American Institute of Aeronautics and Astronautics
|
1997
|
|
|
|
| 1034 |
|
Method for Structural Model Update Using Dynamically Measured Static Flexibility Matrices
|
Denoyer, K. K
|
American Institute of Aeronautics and Astronautics
|
1997
|
|
|
|
| 1035 |
|
Methods for Calculating the Subsonic Aerodynamic Center of Finite Wings/
|
Rodden, W. P
|
American Institute of Aeronautics and Astronautics
|
2003
|
|
|
|
| 1036 |
|
Methods for Predicting Phenomena in the High-Speed Flow of Gases/
|
Lighthill, M. J
|
American Institute of Aeronautics and Astronautics
|
1900
|
|
|
|
| 1037 |
|
Methods for Visualizing Hypersonic Shock-Wave/Boundary-Layer InteractionUsing Electrical Discharges
|
Nishio, M
|
American Institute of Aeronautics and Astronautics
|
1996
|
|
|
|
| 1038 |
|
Micromechanical Analyses of Instabilities in Braided Glass Textile Composites/
|
Quek, S. C
|
American Institute of Aeronautics and Astronautics
|
2003
|
|
|
|
| 1039 |
|
Micromechanics-Based Modeling of Woven Polymer Matrix Composites/
|
Bednarcyk, B. A
|
American Institute of Aeronautics and Astronautics
|
2003
|
|
|
|
| 1040 |
|
Micromechanics of Composites with Shape Memory Alloy Fibers in Uniform Thermal Fields
|
Birman, V
|
American Institute of Aeronautics and Astronautics
|
1996
|
|
|
|
