Call Number (LC) | Title | Results |
---|---|---|
NAS 1.15:106781 |
Effects of artificial viscosity on the accuracy of high-Reynolds-number k-e turbulence model / Effects of artificial viscosity on the accuracy of high-Reynolds-number [kappa-epsilon] turbulence model |
2 |
NAS 1.15:106782 | The aeroacoustics of supersonic coaxial jets | 1 |
NAS 1.15:106783 | High-temperature optical window design | 1 |
NAS 1.15:106784 | Sensor fault detection and diagnosis simulation of a helicopter engine in an intelligent control framework | 1 |
NAS 1.15:106785 | Technology benefit estimator (T/BEST) user's manual / | 1 |
NAS 1.15:106786 | A Cartesian, cell-based approach for adaptively-refined solutions of the Euler and Navier-Stokes equations | 1 |
NAS 1.15:106787 | Correlation of finite element free vibration predictions using random vibration test data | 1 |
NAS 1.15:106788 | Conceptual design of the space station combustion module | 1 |
NAS 1.15:106789 | Modeling of stress/strain behavior of fiber-reinforced ceramic matrix composites including stress redistribution | 1 |
NAS 1.15:106791 | Statistical analysis of microgravity experiment performance using the "degrees of success" scale | 1 |
NAS 1.15:106792 | On the convergence of local approximations to pseudodifferential operators with applications | 1 |
NAS 1.15:106794 | Auroral interactions with ISSA | 1 |
NAS 1.15:106795 | Nickel hydrogen batteries--an overview | 1 |
NAS 1.15:106796 | Multi-objective decision-making under uncertainty fuzzy logic methods / | 1 |
NAS 1.15:106797 | Summary report of mission acceleration measurements for STS-60, SPACEHAB-2 launched February 11, 1994 | 1 |
NAS 1.15:106798 | Atomic oxygen durability evaluation of the flexible batten for the photovoltaic array mast on Space Station | 1 |
NAS 1.15:106799 | A workshop based simulator for teaching compressible aerodynamics | 1 |
NAS 1.15:106800 | EEsoF MICAD and ACADEMY macro files for coplanar waveguide and finite ground plane coplanar waveguide | 1 |
NAS 1.15:106801 | Thermal analysis of a functionally graded material subject to a thermal gradient using the boundary element method | 1 |
NAS 1.15:106802 | Interactive computer graphics applications for compressible aerodynamics | 1 |