| 21 |
|
Coaxial Jets from Lobed-Mixer Nozzles
|
Ramesh Kumar, R
|
American Institute of Aeronautics and Astronautics
|
1996
|
|
|
|
| 22 |
|
Cold Gas Simulation of a Solid Propellant Rocket Motor
|
Couton, D
|
American Institute of Aeronautics and Astronautics
|
1996
|
|
|
|
| 23 |
|
Combined Laser Doppler Velocimetry and Cross-Wire Anemometry Analysis for Supersonic Turbulent Flow
|
Bowersox, R. D. W
|
American Institute of Aeronautics and Astronautics
|
1996
|
|
|
|
| 24 |
|
Comment on "Acoustic Analogy and Alternative Theories for Jet Noise Prediction" (RF)/
|
Tam, C. K. W
|
American Institute of Aeronautics and Astronautics
|
2003
|
|
|
|
| 25 |
|
Comment on "Application of Wall Functions to Generalized Nonorthogonal Curvilinear Coordinate Systems" (RF)
|
Huang, P. G
|
American Institute of Aeronautics and Astronautics
|
1995
|
|
|
|
| 26 |
|
Comment on "Fuzzy Finite Element Approach for the Analysis Imprecisely Defined System" (RF)
|
Elishakoff, I
|
American Institute of Aeronautics and Astronautics
|
1997
|
|
|
|
| 27 |
|
Comment on "Laminar Boundary Layers Subjected to High-Frequency Travelling-Wave Fluctuations"
|
Horton, H. P
|
American Institute of Aeronautics and Astronautics
|
1996
|
|
|
|
| 28 |
|
Comment on "Laminar Flow Past Three Closely Spaced Monodisperse Spheres or Nonevaporating Drops"
|
Pitt, M. J
|
American Institute of Aeronautics and Astronautics
|
1996
|
|
|
|
| 29 |
|
Comment on "Large-Eddy Simulation of a Turbulent Compressible Round Jet" vis-a-vis Lighthill's Theory of Jet Noise (RF)/
|
Ribner, H. S
|
American Institute of Aeronautics and Astronautics
|
2003
|
|
|
|
| 30 |
|
Comment on "New Similarity Solutions for Hypersonic Boundary Layers withApplication to Inlet Flows", Part 1
|
Pike, J
|
American Institute of Aeronautics and Astronautics
|
1996
|
|
|
|
| 31 |
|
Comment on "Penalized Weighted Residual Method for the Initial Value Problem" (RF)
|
Baruch, M
|
American Institute of Aeronautics and Astronautics
|
1997
|
|
|
|
| 32 |
|
Comment on "Rise of Total Pressure in Frictional Flow" (RF)
|
Van Oudheusden, B. W
|
American Institute of Aeronautics and Astronautics
|
1996
|
|
|
|
| 33 |
|
Comment on "Self-Excited Wire Method for the Control of Turbulent MixingLayers"
|
Disimile, P. J
|
American Institute of Aeronautics and Astronautics
|
1996
|
|
|
|
| 34 |
|
Comment on "Structural Damage Identification Using Assigned Partial Eigenstructure" (RF)
|
Baruch, M
|
American Institute of Aeronautics and Astronautics
|
1997
|
|
|
|
| 35 |
|
Comment on "Supersonic Separation with Obstructions" (RF)
|
Oezcan, O
|
American Institute of Aeronautics and Astronautics
|
1997
|
|
|
|
| 36 |
|
Comment on the Vorticity Jump Across a Shock Wave (RF)
|
Isom, M. P
|
American Institute of Aeronautics and Astronautics
|
1996
|
|
|
|
| 37 |
|
Comment on the Vorticity Jump Across a Shock Wave (RF): Reply
|
Emanuel, G
|
American Institute of Aeronautics and Astronautics
|
1996
|
|
|
|
| 38 |
|
Comment on "Vibration and Buckling of Flexible Rotating Beams" (RF)
|
Flax, A. H
|
American Institute of Aeronautics and Astronautics
|
1996
|
|
|
|
| 39 |
|
Comment on "Vibration and Buckling of Flexible Rotating Beams" (RF): Reply
|
Eick, C. D
|
American Institute of Aeronautics and Astronautics
|
1996
|
|
|
|
| 40 |
|
Compact Methodology for Computing Limit-Cycle Oscillations in Aeroelasticity/
|
Epureanu, B. I
|
American Institute of Aeronautics and Astronautics
|
2003
|
|
|
|