| Call Number (LC) | Title | Results |
|---|---|---|
| NAS 1.26:166122/REV | Correction, improvement and model verification of CARE III, version 3 | 1 |
| NAS 1.26:166268 | Study of aerodynamic technology for single-cruise-engine V/STOL fighter/attack aircraft phase I, final report / | 1 |
| NAS 1.26:166269 | Study of aerodynamic technology for single-cruise-engine V/STOL fighter/attack aircraft phase I / | 1 |
| NAS 1.26:166271 | Study of aerodynamic technology for single-cruise-engine V/STOL fighter/attack aircraft final report / | 1 |
| NAS 1.26:166309 | UH-60A Black Hawk engineering simulation program | 1 |
| NAS 1.26:166437 | Speed benefits of tilt-rotor designs for LHX | 1 |
| NAS 1.26:166444 | Integrated technology rotor/flight research rotor (ITR/FRR) concept definition | 1 |
| NAS 1.26:166445 | Integrated technology rotor/flight research rotor (ITR/FRR) concept definition | 1 |
| NAS 1.26:166447 | Integrated technology rotor/flight research rotor hub concept definition / | 2 |
| NAS 1.26:166462 | Addressee errors in ATC communications the call sign problem / | 1 |
| NAS 1.26:166463 |
A dawn to dusk electric field in the Jovian magnetosphere / A dawn to dusk electric field in the jovian magnetosphere / |
2 |
| NAS 1.26:166464 | Morphology and movements of polarization features on Venus : final report / | 2 |
| NAS 1.26:166474 | Automation, supervisory control and workload in flight management / | 2 |
| NAS 1.26:166479 | Investigation to advance prediction techniques of the low-speed aerodynamics of V/STOL aircraft / | 1 |
| NAS 1.26:166482 | An experimental investigation of circulation control flow fields using holographic interferometry | 1 |
| NAS 1.26:166491 | Development of V/STOL methodology based on a higher order panel method | 1 |
| NAS 1.26:166510 | FAR IR spectroscopy of the galactic center neutral and ionized gas in the central 10 pc of the galaxy / | 1 |
| NAS 1.26:166528 | A computer program for the calculation of three-dimensional transonic nacelle/inlet flowfields | 1 |
| NAS 1.26:166529 | A grid-embedding transonic flow analysis computer program for wing/nacelle configurations | 1 |
| NAS 1.26:166531 | Universal single level implicit algorithm for gasdynamics / | 2 |
