| 1361 |
|
Stability Theory for a Pair of Trailing Vortices/
|
Crow, S. C
|
American Institute of Aeronautics and Astronautics
|
1900
|
|
|
|
| 1362 |
|
Stabilization of a Nozzle Boundary Layer by Local Surface Heating
|
Demetriades, A
|
American Institute of Aeronautics and Astronautics
|
1996
|
|
|
|
| 1363 |
|
State-Space Modeling of Aerodynamic Forces on Plate Using Singular ValueDecomposition (TN)
|
Frampton, K. D
|
American Institute of Aeronautics and Astronautics
|
1996
|
|
|
|
| 1364 |
|
Static Collapse of Elastic Circular Arches
|
Knight, N. F
|
American Institute of Aeronautics and Astronautics
|
1997
|
|
|
|
| 1365 |
|
Statistical Experimentation Methods for Achieving Affordable Concurrent Systems Design
|
Chen, W
|
American Institute of Aeronautics and Astronautics
|
1997
|
|
|
|
| 1366 |
|
Statistical Model of Multicomponent-Fuel Drop Evaporation for Many-Drop Flow Simulations/
|
Harstad, K. G
|
American Institute of Aeronautics and Astronautics
|
2003
|
|
|
|
| 1367 |
|
Statistical Saturation of Buoyant Flow Induced by a Fluctuating Acceleration
|
Thomson, J. R
|
American Institute of Aeronautics and Astronautics
|
1996
|
|
|
|
| 1368 |
|
Status of Unsteady Aerodynamic Prediction for Flutter of High-Performance Aircraft/
|
Yurkovich, R
|
American Institute of Aeronautics and Astronautics
|
2003
|
|
|
|
| 1369 |
|
Step Response of Pressure-Sensitive Paints
|
Carroll, B. F
|
American Institute of Aeronautics and Astronautics
|
1996
|
|
|
|
| 1370 |
|
Step-Size Independent Approach for Multidisciplinary Sensitivity Analysis/
|
Newman, J. C
|
American Institute of Aeronautics and Astronautics
|
2003
|
|
|
|
| 1371 |
|
Stiffness Matrix Adjustment Using Incomplete Measured Modes
|
Zhang, O
|
American Institute of Aeronautics and Astronautics
|
1997
|
|
|
|
| 1372 |
|
Stochastic Inlet Conditions for Large-Eddy Simulation of a Fully Turbulent Jet/
|
Glaze, D. J
|
American Institute of Aeronautics and Astronautics
|
2003
|
|
|
|
| 1373 |
|
Stochastic Optimization Using the Stochastic Preconditioned Conjugated Gradient Method
|
Oakley, D. R
|
American Institute of Aeronautics and Astronautics
|
1996
|
|
|
|
| 1374 |
|
Strain-Rate Effects on Unidirectional Carbon-Fiber Composites/
|
Salvi, A. G
|
American Institute of Aeronautics and Astronautics
|
2003
|
|
|
|
| 1375 |
|
Stress and Failure Analysis for Cross-Piled Curved Composite Laminates (TN)
|
Watanabe, N
|
American Institute of Aeronautics and Astronautics
|
1995
|
|
|
|
| 1376 |
|
Stress Fields in General Composite Laminates
|
Davi, G
|
American Institute of Aeronautics and Astronautics
|
1996
|
|
|
|
| 1377 |
|
Structural Damage Detection Using Real-Time Modal Parameter Identification Algorithm
|
Lim, T. W
|
American Institute of Aeronautics and Astronautics
|
1996
|
|
|
|
| 1378 |
|
Structural Damage Identification Using Assigned Partial Eigenstructure
|
Cobb, R. G
|
American Institute of Aeronautics and Astronautics
|
1997
|
|
|
|
| 1379 |
|
Structural Dynamic Frequency Response Using Combined Direct and Adjoint Reduced-Order Approximations/
|
Livne, E
|
American Institute of Aeronautics and Astronautics
|
1900
|
|
|
|
| 1380 |
|
STRUCTURAL MECHANICS AND MATERIALS - Almost-Sure Stochastic Stability of Viscoelastic Plates in Supersonic Flow/
|
Ariaratnam, S T
|
American Institute of Aeronautics and Astronautics
|
2001
|
|
|
|