| Call Number (LC) | Title | Results |
|---|---|---|
| NAS 1.60:1772 | Improved method for calculating transonic velocities on blade-to-blade stream surfaces of a turbomachine / | 1 |
| NAS 1.60:1773 | Kinematic properties of the helicopter in coordinated turns / | 1 |
| NAS 1.60:1775 |
Vibration characteristics of a steadily rotating slender ring / Vibration characteristics of a steadily rotating slender ring |
2 |
| NAS 1.60:1776 | Simulator study of conventional general aviation instrument displays in path-following tasks with emphasis on pilot-induced oscillations / | 1 |
| NAS 1.60:1777 |
Leading-edge deflection optimization for a highly swept arrow-wing configuration / Leading-edge deflection optimization for a highly swept arrow-wing configuration |
2 |
| NAS 1.60:1778 | Aeropropulsive characteristics of twin nonaxisymmetric vectoring nozzles installed with forward swept and aft-swept wings / | 1 |
| NAS 1.60:1779 |
Comparison of Space Shuttle Orbiter low-speed static stability and control derivatives obtained from wind-tunnel and approach and landing flight tests / Comparison of space shuttle orbiter low-speed static stability and control derivatives obtained from wind-tunnel and approach and landing flight tests |
2 |
| NAS 1.60:1780 |
Cold-air investigation of first state of 4 1/2-stage, fan-drive turbine with average stage-loading factor of 4.66 / Cold-air investigation of first state of 4 1/2-stage, fan-drive turbine with average stage-loading factor of 4.66 |
2 |
| NAS 1.60:1781 | Creep and residual mechanical properties of cast superalloys and oxide dispersion stengthened alloys | 1 |
| NAS 1.60:1782 |
Flight evaluation of a simplified gross thrust calculation technique using an F100 turbofan engine in an F-15 airplane / Flight evaluation of a simplified gross thrust calculation technique using an F100 turbofan engine in an F-15 airplane |
2 |
| NAS 1.60:1783 |
Aerothermal environment in chordwise gaps between split elevons at Mach 6.8 / Aerothermal environment in chordwise gaps between split elevons at Mach 6.8 |
2 |
| NAS 1.60:1784 |
Numerical solutions of the Navier-Stokes equations for transonic afterbody flows / Numerical solutions of the Navier-Stokes equations for transonic afterbody flows |
2 |
| NAS 1.60:1785 |
Tests of graphite/polyimide sandwich panels in uniaxial edgewise compression Tests of graphite/polyimide sandwich panels in uniaxial edgewise compression / |
2 |
| NAS 1.60:1787 |
A study of the sonic-boom characteristics of a blunt body at a Mach number of 6 / A study of the sonic-boom characteristics of a blunt body at a Mach number of 6 |
2 |
| NAS 1.60:1788/v.1-2 | Collected reprints / | 1 |
| NAS 1.60:1789 |
Wind-tunnel measurements and comparison with flight of the boundary layer and heat transfer on a hollow cylinder at Mach 3 / Wind-tunnel measurements and comparison with flight of the boundary layer and heat transfer on a hollow cylinder at Mach 3 |
2 |
| NAS 1.60:1790 |
Temporal and spatial inconsistencies of time-split finite-difference schemes / Temporal and spatial inconsistencies of time-split finite-difference schemes |
2 |
| NAS 1.60:1791 |
Capillary and acceleration wave breakup of liquid jets in axial-flow airstreams / Capillary and acceleration wave breakup of liquid jets in axial-flow airstreams |
2 |
| NAS 1.60:1792 | Some flow phenomena associated with aligned, sequential apertures with borda-type inlets / | 2 |
| NAS 1.60:1793 | Determination of the hypersonic-continuum/rarefield-flow drag coefficient of the Viking Lander Capsule 1 aeroshell from flight data / | 1 |
