191 |
|
Parallel Adaptive Finite Element Euler Flow Solver for Rotary Wing Aerodynamics
|
Bottasso, C. L
|
American Institute of Aeronautics and Astronautics
|
1997
|
|
|
192 |
|
Nozzle Thrust Optimization While Reducing Jet Noise
|
Seiner, J. M
|
American Institute of Aeronautics and Astronautics
|
1997
|
|
|
193 |
|
Efficient Computation of Eigenvector Sensitivities for Structural Dynamics
|
Alvin, K. F
|
American Institute of Aeronautics and Astronautics
|
1997
|
|
|
194 |
|
Vibrations of Elastically Restrained Nonuniform Beams with Arbitrary Pretwist
|
Lin, S. M
|
American Institute of Aeronautics and Astronautics
|
1997
|
|
|
195 |
|
Model Update Using Modal Contribution to Static Flexibility Error
|
Denoyer, K. K
|
American Institute of Aeronautics and Astronautics
|
1997
|
|
|
196 |
|
Quantitative Prediction of Thermomechanical Coupling Effect in Thermo-Elasto-Viscoplastic Composite Materials
|
Shin, E.-S
|
American Institute of Aeronautics and Astronautics
|
1997
|
|
|
197 |
|
Geometrically Nonlinear Theory of Multilayered Plates with Interlayer Slips
|
Di Sciuva, M
|
American Institute of Aeronautics and Astronautics
|
1997
|
|
|
198 |
|
Adaptive Topology Optimization of Shell Structures
|
Maute, K
|
American Institute of Aeronautics and Astronautics
|
1997
|
|
|
199 |
|
Flow Model for Predicting Normal Shock Wave Induced Vortex Breakdown
|
Smart, M. K
|
American Institute of Aeronautics and Astronautics
|
1997
|
|
|
200 |
|
Boundary Integral Formulation for Composite Laminates in Torsion
|
Davi, G
|
American Institute of Aeronautics and Astronautics
|
1997
|
|
|