Call Number (LC) | Title | Results |
---|---|---|
NAS 1.15:104122 | User's manual for MacPASCO | 1 |
NAS 1.15:104123 | A relative-intensity two-color phosphor thermography system | 1 |
NAS 1.15:104124 | Kinematics of the six-degree-of-freedom force-reflecting Kraft Master | 1 |
NAS 1.15:104125 | Flapping inertia for selected rotor blades | 1 |
NAS 1.15:104126 | Large angle transient dynamics (LATDYN) documentation post-processor manual / | 1 |
NAS 1.15:104128 | Global change technology architecture trade study / | 1 |
NAS 1.15:104131 | Effect of fiber-matrix debonding on notched strength of titanium metal matrix composites | 1 |
NAS 1.15:104132 | Constant amplitude and post-overload fatigue crack growth behavior in PM aluminum alloy AA 8009 | 1 |
NAS 1.15:104133 |
Improved compression molding technology for continuous fiber reinforced composite laminates Part 2: AS-4/Polyimidesulfone prepreg system / Improved compression molding technology for continuous fiber reinforced composite laminates. Part 2: AS-4/Polyimidesulfone prepreg system |
2 |
NAS 1.15:104134 | Helicopter main-rotor speed effects a comparison of predicted ranges of detection from the aural detection program ICHIN and the electronic detection program ARCAS / | 1 |
NAS 1.15:104137 | Unstructured-grid methods development, lessons learned | 1 |
NAS 1.15:104138 | Maximized gust loads for a nonlinear airplane using matched filter theory and constrained optimization | 1 |
NAS 1.15:104139 | User's guide for a "flat wake" rotor inflow/wake velocity prediction code, "down" | 1 |
NAS 1.15:104140 | An automated thermal vacuum test system for use in environmental testing of flight systems and components | 1 |
NAS 1.15:104141 | Prediction of matrix fatigue crack initiation in notched SCS-6/Ti-15-3 metal matrix composites | 1 |
NAS 1.15:104142 | Investigation of the aeroelastic stability of the AFW wind-tunnel model using CAP-TSD | 1 |
NAS 1.15:104143 | Unstructured-grid methods development for unsteady aerodynamic and aeroelastic analysis | 1 |
NAS 1.15:104144 | Conceptual design and structural analysis of the spectroscopy of the atmosphere using far infrared emission (safire) instrument | 1 |
NAS 1.15:104145 | On simple aerodynamic sensitivity derivatives for use in interdisciplinary optimization | 1 |
NAS 1.15:104146 | Technical activities of the Configuration Aeroelasticity Branch | 1 |