| Call Number (LC) | Title | Results |
|---|---|---|
| NAS 1.15:208111 | Accuracy of aerodynamic model parameters estimated from flight test data | 1 |
| NAS 1.15:208121 | Buckling analysis of anisotropic curved panels and shells with variable curvature | 1 |
| NAS 1.15:208122 | Damage characteristics and residual strength of composite sandwaich panels impacted with and without compression loading presented at the 39th AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics and Materials Conference, session no. 15-damage tolerance : Long Beach, California, April 20-23, 1998 / | 1 |
| NAS 1.15:208123 | Influence of impactor mass on the damage characteristics and failure strength of laminated composite plates presented at the 39th AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics and Materials Conference : Long Beach, California, April 20-23, 1998 / | 1 |
| NAS 1.15:208124 | Effect of curvature on the impact damage characteristics and residual strength of composite plates | 1 |
| NAS 1.15:208126 | Nonlinear analysis of the space shuttle superlightweight LO₂ tank presented at the 39th AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics, and Material Conference : Long Beach, California, April 20-23, 1998 / | 1 |
| NAS 1.15:208127 | Nonlinear analysis of the space shuttle superlightweight LO₂ tank presented at the 39th AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics, and Material Conference : Long Beach, California, April 20-23, 1998 / | 1 |
| NAS 1.15:208129 | Aircraft structural mass property prediction using conceptual-level structural analysis | 1 |
| NAS 1.15:208131 | The use of a satellite climatological data set to infer large scale three dimensional flow characteristics | 1 |
| NAS 1.15:208134 | Rate and gain limitations of MSGC's and MGC's combined with GEM and other preamplification structures | 1 |
| NAS 1.15:208137 | Overview of the International Space Station System level trace contaminant injection test | 1 |
| NAS 1.15:208139 | Analysis of aerospike plume induced base-heating environment | 1 |
| NAS 1.15:208141 | The 1997 HST Calibration Workshop, with a new generation of instruments proceedings of a workshop held at the Space Telescope Science Institute, Baltimore, Maryland, September 22-24, 1997 / | 1 |
| NAS 1.15:208142 | Progressive fracture and damage tolerance of composite pressure vessels | 1 |
| NAS 1.15:208146 | Effect of velocity and temperature distribution at the hole exit on film cooling of turbine blades | 1 |
| NAS 1.15:208150 | The Aircraft Morphing Program | 1 |
| NAS 1.15:208169 | Microgravity vibration control and civil applications | 1 |
| NAS 1.15:208181 |
Mirror material properties compiled for preliminary design of the next generation space telescope (30 to 294 Kelvin) / Mirror material properties compiled for preliminary design of the Next Generation Space Telescope (30 to 294 Kelvin) |
2 |
| NAS 1.15:208191 | Response of composite fuselage sandwich side panels subjected to internal pressure and axial tension | 1 |
| NAS 1.15:208194 |
Thruster injector faceplate testing in support of the aerojet rocket-based combined cycle (RBCC) concept / Thruster injector faceplate testing in support of the aerojet Rocket-based combined cycle (RBCC) concept |
2 |
