Call Number (LC) | Title | Results |
---|---|---|
NAS 1.15:85888 | Structure-activity correlations for organophosphorus ester anticholinesterases | 1 |
NAS 1.15:85889 | Turbulence modeling | 1 |
NAS 1.15:85890 |
A mathematical model of the UH-60 helicopter Mathematical model of the UH-60 helicopter |
2 |
NAS 1.15:85892 | Hover test of a full-scale hingeless helicopter rotor: Aeroelastic stability, performance and loads data | 1 |
NAS 1.15:85893 | Physical aspects of computing the flow of a viscous fluid | 1 |
NAS 1.15:85894 | Navier-Stokes calculations for the vortex of a rotor in hover | 1 |
NAS 1.15:85895 | In-flight acoustic testing techniques using the YO-3A Acoustic Research Aircraft | 1 |
NAS 1.15:85896 | Hardware/software simulation for the video tracking system of the Kuiper Airborne Observatory telescope | 1 |
NAS 1.15:85898 | Application of a fractional-step method to incompressible Navier-Stokes equation | 1 |
NAS 1.15:85899 |
Compressible Navier-Stokes code for turbulent flow modeling A compressible Navier-Stokes code for turbulent flow modeling |
2 |
NAS 1.15:85900 | Effect of control logic modifications on airstart performance of F100 engine model derivative engines in an F-15 airplane | 1 |
NAS 1.15:85901 | Flight investigation of various control inputs intended for parameter estimation | 1 |
NAS 1.15:85902 | Preliminary flight test results of the F100 EMD engine in an F-15 airplane | 1 |
NAS 1.15:85903 | Simulator evaluation of a remotely piloted vehicle lateral landing task using a visual display | 1 |
NAS 1.15:85904 | Impacts of Space Shuttle thermal protection system tile on F-15 aircraft vertical tile | 1 |
NAS 1.15:85905 | More than you may want to know about maximum likelihood estimation | 1 |
NAS 1.15:85906 | Ground vibration test results for Drones for Aerodynamic and Structural Testing (DAST)/Aeroelastic Research Wing (ARW-1R) aircraft | 1 |
NAS 1.15:85907 | Thermal response of space shuttle wing during reentry heating | 1 |
NAS 1.15:85908 | Software control and system configuration management a systems-wide approach / | 1 |
NAS 1.15:85909 | X-29A longitudinal and directional force and moment supplemental transonic wind tunnel test results | 1 |