| Call Number (LC) | Title | Results |
|---|---|---|
| NAS 1.60:1699 | Crash tests of four identical high-wing single-engine airplanes / | 1 |
| NAS 1.60:1700 |
Development of the reentry flight dynamics simulator for evaluation of space shuttle orbiter entry systems Development of the reentry flight dynamics simulator for evaluation of Space Shuttle Orbiter entry systems / |
2 |
| NAS 1.60:1701 |
Aerodynamic characteristics of three helicopter rotor airfoil sections at Reynolds numbers from model scale to full scale at Mach numbers from 0.35 to 0.90 Aerodynamic characteristics of three helicopter rotor airfoil sections at Reynolds numbers from model scale to full scale at Mach numbers from 0.35 to 0.90 / |
2 |
| NAS 1.60:1702 | Release mechanism for releasing and reattaching experiments on the space shuttle / | 1 |
| NAS 1.60:1703 |
Aerothermal analysis of a wing-elevon cove with variable leakage / Aerothermal analysis of a wing-elevon cove with variable leakage |
2 |
| NAS 1.60:1704 | The effect of throat contouring on two-dimensional converging-diverging nozzles at static conditions / | 1 |
| NAS 1.60:1705 | CAS2D - FORTRAN program for nonrotating blade-to-blade, steady potential transonic cascade flows / | 1 |
| NAS 1.60:1706 | Annoyance due to multiple airplane noise exposure / | 1 |
| NAS 1.60:1707 | Fracture toughness of boron/aluminum laminates with various proportions of 0° and ±45̊ plies | 1 |
| NAS 1.60:1708 |
Off-design performance loss model for radial turbines with pivoting, variable-area stators / Off-design performance loss model for radial turbines with pivoting, variable-area stators |
2 |
| NAS 1.60:1709 | MARS 1414 recorder environmental tests / | 1 |
| NAS 1.60:1710 | Life analysis of multiroller planetary traction drive / | 1 |
| NAS 1.60:1711 |
Cognitive issues in head-up displays Cognitive issues in head-up displays / |
2 |
| NAS 1.60:1712 | Effects of conversation interference on annoyance due to aircraft noise / | 1 |
| NAS 1.60:1713 |
Low-pressure performance of annular, high-pressure (40-atm), high-temperature, (2480 K) combustion system Low-pressure performance of annular, high-pressure (40-atm), high-temperature, (2480 K) combustion system / |
2 |
| NAS 1.60:1714 | Lubrication of optimized-design tapered-roller bearings to 2.4 million DN / | 1 |
| NAS 1.60:1715 | The time-space relationships of the data points (pixels) of the thematic mapper and multispectral scanner of "The myth of simultaneity" / | 1 |
| NAS 1.60:1716 | Effect of hole geometry and electric-discharge machining (EDM) on airflow rates through small-diameter holes in turbine-blade material / | 1 |
| NAS 1.60:1717 |
Development and test results of a flight management algorithm for fuel-conservation descents in a time-based metered traffic environment Development and test results of a flight management algorithm for fuel-conservation descents in a time-based metered traffic environment / |
2 |
| NAS 1.60:1718 |
Estimation of wing nonlinear aerodynamic characteristics at supersonic speeds Estimation of wing nonlinear aerodynamic characteristics at supersonic speeds / |
2 |
