Call Number (LC) Title Results
Y 3.N 21/5:11/E99 Effect of aromatics and spark advance on thermal efficiency / 1
Y 3.N 21/5:11/L-126 Evaluation of the induced-velocity field of an idealized helicopter rotor / 1
Y 3.N 21/5:11/L-164 Analysis of factors affecting net lift increment attainable with trailing-edge split flaps on tailless airplanes / 1
Y 3.N 21/5:11/L1 Wind-tunnel calibration and correction procedures for three-dimensional models / 1
Y 3.N 21/5:11/L10 An analysis of the fatigue life of an airplane wing structure under overload conditions / 1
Y 3.N 21/5:11/L100 Maximum rates of control motion obtained from ground tests / 1
Y 3.N 21/5:11/L101 Static-thrust tests of six rotor-blade designs on a helicopter in the Langley full-scale tunnel / 1
Y 3.N 21/5:11/L102 An approximate determination of the power required to move control surfaces as related to control-booster design / 1
Y 3.N 21/5:11/L103 The effect of lateral area on the lateral stability and control characteristics of an airplane as determined by tests of a model in the Langley free-flight tunnel / 1
Y 3.N 21/5:11/L104 Strain measurements and strength tests of 25-inch diagonal-tension beams with single uprights / 1
Y 3.N 21/5:11/L105 Wind-tunnel tests of a blunt-nose aileron with beveled trailing edge on an NACA 66(215)-216 airfoil with several modifications of aileron nose and adjacent airfoil contour / 1
Y 3.N 21/5:11/L106 Shear-lag tests of a box beam with a highly cambered cover in tension / 1
Y 3.N 21/5:11/L107 Tables and charts for the evaluation of profile drag from wake surveys at high subsonic speeds / 1
Y 3.N 21/5:11/L108 A summary of drag results from recent Langley full-scale-tunnel tests of Army and Navy airplanes / 1
Y 3.N 21/5:11/L109 Langley full-scale tunnel investigation of the factors affecting the directional stability and trim characteristics of a fighter-type airplane / 1
Y 3.N 21/5:11/L11 Application of a numerical procedure to stress analysis of stringer-reinforced panels / 1
Y 3.N 21/5:11/L110 Charts for estimation of the characteristics of a helicopter rotor in forward flight. : 1 - Profile drag-lift ratio for untwisted rectangular blades / 1
Y 3.N 21/5:11/L111 Effect of elevator-profile modifications and trailing-edge strips on elevator hinge-moment and other aerodynamic characteristics of a full-scale horizontal tail surface / 1
Y 3.N 21/5:11/L112 A method for studying the hunting oscillations of an airplane with a simple type of automatic control / 1
Y 3.N 21/5:11/L113 The conformal transformation of an airfoil into a straight line and its application to the inverse problem of airfoil theory / 1