Call Number (LC) | Title | Results |
---|---|---|
NAS 1.15:104173 | NASA/DoD aerospace knowledge diffusion research project. | 1 |
NAS 1.15:104174 | The multi-attribute task battery for human operator workload and strategic behavior research | 1 |
NAS 1.15:104175 | A pc-based bus monitor program for use with the Transport Systems Research Vehicle RS-232 communication interfaces | 1 |
NAS 1.15:104176 | Expanded serial communication capability for the Transport Systems Research Vehicle laptop computers | 1 |
NAS 1.15:104177 | Neural network modeling of nonlinear systems based on Volterra series extension of a linear model | 1 |
NAS 1.15:104178 | Structure-property study of keto-ether polyimides | 1 |
NAS 1.15:104179 | Quantifiable figures of merit for nuclear thermal propulsion report of the Nuclear Propulsion Mission Analysis Figures of Merit subpanel / | 1 |
NAS 1.15:104180 | The benchmark aeroelastic models program description and highlights of initial results / | 1 |
NAS 1.15:104181 |
Delamination behavior of quasi-isotropic graphite epoxy laminates subjected to tension and torsion loads Delamination behavior of quasi-isotropic graphite epoxy laminates subjected to tension and torsion loads / |
2 |
NAS 1.15:104184 | Thermal/structural analysis of a transpiration cooled nozzle | 1 |
NAS 1.15:104186 | A fast implicit upwind solution algorithm for three-dimensional unstructured dynamic meshes | 1 |
NAS 1.15:104187 | The propagation characteristics of the plate modes of acoustic emission waves in thin aluminium plates and thin graphite/epoxy composite plates and tubes | 1 |
NAS 1.15:104189 | The use of impact force as a scale parameter for the impact response of composite laminates | 1 |
NAS 1.15:104190 | Application of program LAURA to perfect gas shock tube flows a parametric study / | 1 |
NAS 1.15:104191 | Current status of computational methods for transonic unsteady aerodynamics and aeroelastic applications | 1 |
NAS 1.15:104192 | The NASA/industry Design Analysis Methods for Vibrations (DAMVIBS) program accomplishments and contributions / | 1 |
NAS 1.15:104193 | Experiences at Langley Research Center in the application of optimization techniques to helicopter airframes for vibration reduction | 1 |
NAS 1.15:104194 | Optimizing tuning masses for helicopter rotor blade vibration reduction including computed airloads and comparison with test data | 1 |
NAS 1.15:104195 | Imide/arylene ether copolymers with pendent trifluoromethyl groups | 1 |
NAS 1.15:104196 | Formal design and verification of a reliable computing platform for real-time control phase 2 results / | 1 |