| 21 |
|
Accurate Development of Leading-Edge Vortex Using an Embedded Conical Grid
|
Kumar, A
|
American Institute of Aeronautics and Astronautics
|
1996
|
|
|
|
| 22 |
|
Accurate Multiblock Navier-Stokes Solver for Complex Aerodynamic Configurations/
|
Epstein, B
|
American Institute of Aeronautics and Astronautics
|
2003
|
|
|
|
| 23 |
|
Accurate Numerical Integration of State-Space Models for Aeroelastic Systems with Free Play
|
Conner, M. D
|
American Institute of Aeronautics and Astronautics
|
1996
|
|
|
|
| 24 |
|
Acoustic Response of Droplet Flames to Pressure Oscillations
|
Sohn, C. H
|
American Institute of Aeronautics and Astronautics
|
1996
|
|
|
|
| 25 |
|
Active Control of Panel Oscillation Induced by Accelerating Boundary Layer and Sound
|
Maestrello, L
|
American Institute of Aeronautics and Astronautics
|
1997
|
|
|
|
| 26 |
|
Active Panel Flutter Suppression Using Self-Sensing Piezoactuators
|
Doengi, F
|
American Institute of Aeronautics and Astronautics
|
1996
|
|
|
|
| 27 |
|
Active Transparent Stall Control System for Air Vehicles/
|
Patel, M. P
|
American Institute of Aeronautics and Astronautics
|
2003
|
|
|
|
| 28 |
|
Actuator with Built-In Viscous Damping for Isolation and Structural Control
|
Hyde, T. T
|
American Institute of Aeronautics and Astronautics
|
1996
|
|
|
|
| 29 |
|
Adaptive Finite Volume Upwind Approaches for Aeroacoustic Computations
|
Hwang, C. J
|
American Institute of Aeronautics and Astronautics
|
1997
|
|
|
|
| 30 |
|
Adaptive Harmonic Balance Solutions to Euler's Equation/
|
Maple, R. C
|
American Institute of Aeronautics and Astronautics
|
2003
|
|
|
|
| 31 |
|
Adaptive Monte Carlo Simulation for Time-Variant Reliability Analysis ofBrittle Structures
|
Mahadevan, S
|
American Institute of Aeronautics and Astronautics
|
1997
|
|
|
|
| 32 |
|
Adaptive Prismatic-Tetrahedral Grid Refinement and Redistribution for Viscous Flows
|
Parthasarathy, V
|
American Institute of Aeronautics and Astronautics
|
1996
|
|
|
|
| 33 |
|
Adaptive Remeshing for the k-�Model of Turbulence
|
Pelletier, D
|
American Institute of Aeronautics and Astronautics
|
1997
|
|
|
|
| 34 |
|
Adaptive Topology Optimization of Shell Structures
|
Maute, K
|
American Institute of Aeronautics and Astronautics
|
1997
|
|
|
|
| 35 |
|
Adaptive Unstructured Grid Generation for Viscous Flow Applications
|
Marcum, D. L
|
American Institute of Aeronautics and Astronautics
|
1996
|
|
|
|
| 36 |
|
Adaptivity, Sensitivity, and Uncertainty: Toward Standards of Good Practice in Computational Fluid Dynamics/
|
Pelletier, D
|
American Institute of Aeronautics and Astronautics
|
2003
|
|
|
|
| 37 |
|
Advantages of a Bristled Wing as a Rotary Wing/
|
Sunada, S
|
American Institute of Aeronautics and Astronautics
|
2003
|
|
|
|
| 38 |
|
Aeroacoustic Boundary Element Method Using Analytical/Numerical Matching
|
Epstein, R. J
|
American Institute of Aeronautics and Astronautics
|
1997
|
|
|
|
| 39 |
|
Aeroacoustic Properties of a Supersonic Diamond-Shaped Jet
|
Alvi, F. S
|
American Institute of Aeronautics and Astronautics
|
1996
|
|
|
|
| 40 |
|
Aerodynamically Accurate Three-Dimensional Navier-Stokes Method (TN)
|
Epstein, B
|
American Institute of Aeronautics and Astronautics
|
1997
|
|
|
|