401 |
|
Near-Wall Integration of Reynolds Stress Turbulence Closures with No Wall Damping
|
Speziale, C. G
|
American Institute of Aeronautics and Astronautics
|
1996
|
|
|
402 |
|
Modeling Nonaxisymmetric Off-Design Shapes of Large Scientific Balloons
|
Baginski, F
|
American Institute of Aeronautics and Astronautics
|
1996
|
|
|
403 |
|
Atomic Oxygen Line Shape Measurement at 130 nm with Raman-Shifted Laser
|
Meyer, S. A
|
American Institute of Aeronautics and Astronautics
|
1996
|
|
|
404 |
|
New Method for Deriving Eigenvalue Rate with Respect to Support Location
|
Liu, Z
|
American Institute of Aeronautics and Astronautics
|
1996
|
|
|
405 |
|
Tone Excitation of a Supersonic Bounded Shear Layer
|
Ramaswamy, M
|
American Institute of Aeronautics and Astronautics
|
1996
|
|
|
406 |
|
Law, Virtue, and the Corporation
|
Nesteruk, J.
|
MARQUETTE UNIVERSITY-COLLEGE OF BUSINESS ADM
|
1996
|
|
|
407 |
|
Ballistic Impact Response for Two-Step Braided Three-Dimensional TextileComposites
|
Jenq, S. T
|
American Institute of Aeronautics and Astronautics
|
1996
|
|
|
408 |
|
Postprocess Method Using Displacement Field of Higher Order Laminated Composite Plate Theory
|
Cho, M
|
American Institute of Aeronautics and Astronautics
|
1996
|
|
|
409 |
|
Suppression of Nonlinear Panel Flutter at Supersonic Speeds and ElevatedTemperatures
|
Zhou, R. C
|
American Institute of Aeronautics and Astronautics
|
1996
|
|
|
410 |
|
Infrared Emission from High-Temperature H~2O(upsilon~2): A Diagnostic for Concentration and Temperature
|
Parker, T. E
|
American Institute of Aeronautics and Astronautics
|
1996
|
|
|