| Call Number (LC) | Title | Results |
|---|---|---|
| NAS 1.15:86013 | Detection of submillimeter polarization in the Orion nebula | 1 |
| NAS 1.15:86015 | Fiber optic data bus using frequency division multiplexing (FDM) and an asymmetric coupler | 1 |
| NAS 1.15:86016 | Flow-separation patterns on symmetric forebodies | 1 |
| NAS 1.15:86017 | Ultrareliable, fault-tolerant, control systems a conceptual description / | 1 |
| NAS 1.15:86018 |
Status and prospects of computational fluid dynamics for unsteady transonic viscous flows Status and prospects of computational fluid dynamics for unsteady transonic viscous flows / |
2 |
| NAS 1.15:86019 | The structure of the vorticity field in turbulent channel flow. | 1 |
| NAS 1.15:86020 | On the connection between multigrid and cyclic reduction | 2 |
| NAS 1.15:86021 | Development of computational fluid dynamics at NASA Ames Research Center | 1 |
| NAS 1.15:86022 | Far-infrared photometry of compact extragalactic sources OJ 287 and BL Lac / | 1 |
| NAS 1.15:86023 | Project management techniques for highly integrated programs | 2 |
| NAS 1.15:86024 | In-flight load testing of advanced shuttle thermal protection systems | 2 |
| NAS 1.15:86025 | X-29 flight-research program | 1 |
| NAS 1.15:86026 | Design implications from AFTI/F-16 flight test | 1 |
| NAS 1.15:86028 | Flight test experience with pilot-induced-oscillation suppression filters | 1 |
| NAS 1.15:86029 | Air data position-error calibration using state reconstruction techniques | 1 |
| NAS 1.15:86030 | Comparison of pilot effective time delay for cockpit controllers used on space shuttle and conventional aircraft | 2 |
| NAS 1.15:86031 | Preliminary flight evaluation of F100 engine model derivative airstart capability in an F-15 airplane | 1 |
| NAS 1.15:86033 |
Effect of creep in titanium alloy Ti6Al-4V at elevated temperature on aircraft design and flight test Effect of creep in titanium alloy Ti-6Al-4V at elevated temperature on aircraft design and flight test |
2 |
| NAS 1.15:86034 | Space shuttle pilot-induced-oscillation research testing | 2 |
| NAS 1.15:86035 | A comparison of Wortmann airfoil computer-generated lift and drag polars with flight and wind tunnel results | 1 |
