| Call Number (LC) | Title | Results |
|---|---|---|
| Y 3.N 21/5:6/1052 |
Wind-tunnel investigation of effect of canopies on directional stability characteristics of a single-engine airplane model / Wind-tunnel investigation of effect of canopies on directional stability characteristics of a single-engine airplane model. |
2 |
| Y 3.N 21/5:6/1053 |
Use of ducted head baffles to reduce rear-row cylinder temperatures of an air-cooled aircraft engine. Use of ducted head baffles to reduce rear-row cylinder temperatures of an air-cooled aircraft engine / |
2 |
| Y 3.N 21/5:6/1054 |
Impact strength and flexural properties of laminated plastics at high and low temperatures / Impact strength and flexural properties of laminated plastics at high and low temperatures. |
2 |
| Y 3.N 21/5:6/1055 |
Comparison of two-dimensional air flows about an NACA 0012 airfoil of 1-inch chord at zero lift in open and closed 3-inch jets and corrections for jet-boundary interference / Comparison of two-dimensional air flows about an NACA 0012 airfoil of 1-inch chord at zero lift in open and closed 3-inch jets and corrections for jet-boundary interference. |
2 |
| Y 3.N 21/5:6/1056 |
The Effects of various parameters on the load oat which spray enters the propellers of a flying boat / The effects of various parameters on the load at which spray enters the propellers of a flying boat. |
2 |
| Y 3.N 21/5:6/1057 |
General tank tests of a 1/10-size model of the hull of the Boeing XPBB-1 flying boat - Langley tank model 175 / General tank tests of 1/10-size model of the hull of the Boeing XPBB-1 flying boat - Langley tank model 175. |
2 |
| Y 3.N 21/5:6/1058 |
Strain measurements and strength tests of 25-inch diagonal-tension beams of 75S-T aluminum alloy / Strain measurements and strength tests of 25-inch diagonal-tension beams of 75S-T aluminum alloy. |
2 |
| Y 3.N 21/5:6/1059 |
Effects of tip dihedral on lateral stability and control characteristics as determined by tests of a dynamic model in the Langley free-flight tunnel / Effects of tip dihedral on lateral stability and control characteristics as determined by tests of a dynamic model in the Langley free-flight tunnel. |
2 |
| Y 3.N 21/5:6/1060 |
An investigation of additional requirements for satisfactory elevator control characteristics / An investigation of additional requirements for satisfactory elevator control characteristics. |
2 |
| Y 3.N 21/5:6/1061 |
Wind-tunnel investigation of effect of wing location, power, and flap deflection on effective dihedral of a typical single-engine fighter-airplane model with tail removed / Wind-tunnel investigation of effect of wing location, power, and flap deflection on effective dihedral of a typical single-engine fighter-airplane model with tail removed. |
2 |
| Y 3.N 21/5:6/1062 |
Tank tests to determine the effect of varying design parameters of planing-tail hulls. Tank tests to determine the effect of varying design parameters of planing-tail hulls, 1 - effect of varying length, width, and plan-form taper of afterbody. |
2 |
| Y 3.N 21/5:6/1063 |
Comparison of measured and calculated stresses in built-up beams / Comparison of measured and calculated stresses in built-up beams. |
2 |
| Y 3.N 21/5:6/1064 |
Lifting-surface-theory results for thin elliptic wings of aspect ratio 3 with chordwise loadings corresponding to 0.5-chord plain flap and to parabolic-arc camber / Lifting-surface-theory results for thin elliptic wings of aspect ratio 3 with chordwise loadings corresponding to 0.5-chord plain flap and to parabolic-arc camber. |
2 |
| Y 3.N 21/5:6/1065 |
Consideration of dynamic loads on the vertical tail by the theory of flat yawing maneuvers / Consideration of dynamic loads on the vertical tail by the theory of flat yawing maneuvers. |
2 |
| Y 3.N 21/5:6/1066 |
Stresses around large cut-outs in torsion boxes / Stresses around large cut-outs in torsion boxes. |
2 |
| Y 3.N 21/5:6/1067 | Comparison of several methods of predicting the pressure loss at altitude across a baffled aircraft-engine cylinder / | 1 |
| Y 3.N 21/5:6/1068 | Effects of axial-plane curvature and passage-area variation on flow capacity of radial-discharge impeller with conventional inlet buckets / | 1 |
| Y 3.N 21/5:6/1069 | Effect of the NACA injection impeller on the mixture distribution of a double-row radial aircraft engine / | 1 |
| Y 3.N 21/5:6/1070 | An Empirical equation for the coefficient of heat transfer to a flat surface from a plane heated-air jet directed tangentially to the surface / | 1 |
| Y 3.N 21/5:6/1071 | Wind-tunnel investigation of boundary-layer control by suction on the NACA 653-418, a = 1.0 airfoil section with a 0.29-airfoil-chord double slotted flap / | 1 |
