Call Number (LC) Title Results
Y 3.N 21/5:11/L169 Resume of hinge-moment data for unshielded horn-balanced control surfaces / 1
Y 3.N 21/5:11/L17 Investigation of effect of sideslip on lateral stability characteristics. : 3 - Rectangular low wing on circular fuselage with variations in vertical-tail area and fuselage length with and without horizontal tail surface / 1
Y 3.N 21/5:11/L170 Effect of fabric deflection at high speeds on the aerodynamic characteristics of the horizontal tail surface of an SB2D-1 airplane / 1
Y 3.N 21/5:11/L171 Analysis of available data on the effectiveness of ailerons without exposed overhang balance / 1
Y 3.N 21/5:11/L172 Effect of leakage past aileron nose on aerodynamic characteristics of plain and internally balanced ailerons on NACA 66(215)-216, a = 1.0 airfoil / 1
Y 3.N 21/5:11/L173 Column and plate compressive strengths of aircraft structural materials. : Extruded 75S-T aluminum alloy / 1
Y 3.N 21/5:11/L174 Hinge moments of sealed-internal-balance arrangements for control surfaces. : 1 - Theoretical investigation / 1
Y 3.N 21/5:11/L175 Wind-tunnel investigation of control-surface characteristics. : 21 - Medium and large aerodynamic balances of two nose shapes and a plain overhang used with a 0.40-airfoil-chord flap on an NACA 0009 airfoil / 1
Y 3.N 21/5:11/L176 Tensile tests of NACA and conventional machine-countersunk flush rivets / 1
Y 3.N 21/5:11/L177 Climb and high-speed tests of a Curtiss No. 714-1C2-12 four-blade propeller on the Republic P-47C airplane / 1
Y 3.N 21/5:11/L178 Wind-tunnel investigation of aileron effectiveness of 0.20-airfoil-chord plain ailerons of true airfoil contour on NACA 65(2)-415, 65(3)-418 and 65(4)-421 airfoil sections / 1
Y 3.N 21/5:11/L179 Compressibility effects on heat transfer and pressure drop in smooth cylindrical tubes / 1
Y 3.N 21/5:11/L18 An infrared cloud indicator. : 1 - Analysis of infrared-radiation exchange with tables and chart for calibration of the cloud indicator / 1
Y 3.N 21/5:11/L180 Determination of desirable lengths of Z- and channel-section columns for local-instability tests / 1
Y 3.N 21/5:11/L181 Analysis of vertical-tail loads in rolling pull-out maneuvers / 1
Y 3.N 21/5:11/L182 The relation between spanwise variations in the critical Mach number and spanwise load distributions / 1
Y 3.N 21/5:11/L183 Critical combinations of shear and transverse direct stress for an infinitely long flat plate with edges elastically restrained against rotation / 1
Y 3.N 21/5:11/L184 Experimental verification of the rudder-free stability theory for an airplane model equipped with rudders having negative floating tendency and negligible friction / 1
Y 3.N 21/5:11/L185 Effect of hinge-moment parameters on elevator stick forces in rapid maneuvers / 1
Y 3.N 21/5:11/L186 Wind-tunnel investigation of control-surface characteristics. : 20 - Plain and balanced flaps on an NACA 0009 rectangular semispan tail surface / 1