Call Number (LC) Title Results
Y 3.N 21/5:6/4393 Some static longitudinal stability characteristics of an overlapped-type tandem-rotor helicopter at low airspeeds / 1
Y 3.N 21/5:6/4394 The rate of fatigue-crack propagation in two aluminum alloys / 1
Y 3.N 21/5:6/4395 Use of the kernel function in a three-dimensional flutter analysis with application to a flutter-tested delta-wing model / 1
Y 3.N 21/5:6/4396 A phenomenological theory for the transient creep of metals at elevated temperatures / 1
Y 3.N 21/5:6/4397 Static longitudinal and lateral stability characteristics at low speed of 60 degree sweptback-midwing models having wings with an aspect ratio of 2, 4, or 6 / 1
Y 3.N 21/5:6/4398 Analysis of the creep behavior of a square plate loaded in edge compression / 1
Y 3.N 21/5:6/4399 Relative motion in the terminal phase of interception of a satellite or a ballistic missile / 1
Y 3.N 21/5:6/4400 Measurements of ground-reaction forces and vertical center-of-gravity accelerations of a bomber airplane taxiing over obstacles / 1
Y 3.N 21/5:6/4401 Hydrodynamic impact loads on 30 degree and 60 degree V-step plan-form models with and without dead rise / 1
Y 3.N 21/5:6/4402 Measurements of aerodynamic forces and moments at subsonic speeds on a simplified T-tail oscillating in yaw about the fin midchord / 1
Y 3.N 21/5:6/4403 Tests of ring-stiffened circular cylinders subjected to a transverse shear load / 1
Y 3.N 21/5:6/4404 Effects of propeller position and overlap on the slipstream deflection characteristics of a wing-propeller configuration equipped with a sliding and Fowler flap / 1
Y 3.N 21/5:6/4405 Free-flight investigation to determine the drag of flat- and vee-windshield canopies on a parabolic fuselage with and without transonic indentation between Mach numbers of 0.75 and 1.35 / 1
Y 3.N 21/5:6/4406 Low tire friction and cornering forces on a wet surface / 1
Y 3.N 21/5:6/4407 Effects of ground proximity on the thrust of a simple downard-directed jet beneath a flat surface / 1
Y 3.N 21/5:6/4408 The theory of diffusion in strained systems / 1
Y 3.N 21/5:6/4409 Flight measurements of the vibration experienced by a tandem helicopter in transition, vortex-ring state, landing approach, and yawed flight / 1
Y 3.N 21/5:6/4410 Flight measurements of the vibratory stresses on a propeller designed for an advance ratio of 4.0 and a Mach number of 0.82 / 1
Y 3.N 21/5:6 IND/940 Index of technical notes on aeronautical research. 1
Y 3.N 21/5:6 LIST/947-53 List of Technical notes, 1947-1953. 1