Call Number (LC) Title Results
Y3.N21_5..6_1047 Clamped long rectangular plate under combined axial load and normal pressure. 1
Y3.N21_5..6_1048 Two-dimensional wind-tunnel investigation of low-drag vertical-tail, horizontal-tail, and wing sections equipped with sealed internally balanced control surfaces. 1
Y3.N21_5..6_1049 Analysis of available data on the effects of tabs on control-surface hinge moments. 1
Y3.N21_5..6_1050 Wind-tunnel investigation of end-plate effects of horizontal tails on a vertical tail compared with available theory. 1
Y3.N21_5..6_1051 Preliminary investigation of the loads carried by individual bolts in bolted joints. 1
Y3.N21_5..6_1052 Wind-tunnel investigation of effect of canopies on directional stability characteristics of a single-engine airplane model. 1
Y3.N21_5..6_1053 Use of ducted head baffles to reduce rear-row cylinder temperatures of an air-cooled aircraft engine. 1
Y3.N21_5..6_1054 Impact strength and flexural properties of laminated plastics at high and low temperatures. 1
Y3.N21_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. 1
Y3.N21_5..6_1056 The effects of various parameters on the load at which spray enters the propellers of a flying boat. 1
Y3.N21_5..6_1057 General tank tests of 1/10-size model of the hull of the Boeing XPBB-1 flying boat - Langley tank model 175. 1
Y3.N21_5..6_1058 Strain measurements and strength tests of 25-inch diagonal-tension beams of 75S-T aluminum alloy. 1
Y3.N21_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. 1
Y3.N21_5..6_1060 An investigation of additional requirements for satisfactory elevator control characteristics. 1
Y3.N21_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. 1
Y3.N21_5..6_1062 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. 1
Y3.N21_5..6_1063 Comparison of measured and calculated stresses in built-up beams. 1
Y3.N21_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. 1
Y3.N21_5..6_1065 Consideration of dynamic loads on the vertical tail by the theory of flat yawing maneuvers. 1
Y3.N21_5..6_1066 Stresses around large cut-outs in torsion boxes. 1