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