Call Number (LC) Title Results
Y 3.N 21/5:6/3479 Analysis of the horizontal-tail loads measured in flight on a multiengine jet bomber / 1
Y 3.N 21/5:6/3480 Free-spinning-tunnel investigation of gyroscopic effects of jet-engine rotating parts (or of rotating propellers) on spin and spin recovery / 1
Y 3.N 21/5:6/3481 Wind-tunnel investigation at low speed of effect of size and position of closed air ducts on static longitudinal and static lateral stability characteristics of unswept-midwing models having wings of aspect ratio 2, 4, and 6 / 1
Y 3.N 21/5:6/3482 Supplementary charts for estimating performance of high-performance helicopters / 1
Y 3.N 21/5:6/3483 An analysis of acceleration, airspeed, and gust-velocity data from a four-engine transport airplane in operations on an eastern United States route / 2
Y 3.N 21/5:6/3484 On spectral analysis of runway roughness and loads developed during taxiing / 1
Y 3.N 21/5:6/3485 An approximate solution for axially symmetric flow over a cone with an attached shock wave / 1
Y 3.N 21/5:6/3486 Measurements of turbulent skin friction on a flat plate at transonic speeds / 1
Y 3.N 21/5:6/3487 Acoustic radiation from two-dimensional rectangular cutouts in aerodynamic surfaces / 2
Y 3.N 21/5:6/3488 Some measurements of flow in a rectangular cutout / 1
Y 3.N 21/5:6/3490 Experimental and calculated temperature and mass histories of vaporizing fuel drops / 1
Y 3.N 21/5:6/3491 Experimental investigation of eccentricity ratio, friction, and oil flow of long and short journal bearings with load-number charts / 1
Y 3.N 21/5:6/3492 Determination of inflow distributions from experimental aerodynamic loading and blade-motion data on a model helicopter rotor in hovering and forward flight / 1
Y 3.N 21/5:6/3493 Development of equipment and of experimental techniques for column creep tests / 1
Y 3.N 21/5:6/3494 Sound propagation into the shadow zone in a temperature-stratified atmosphere above a plane boundary / 1
Y 3.N 21/5:6/3495 Failure of materials under combined repeated stresses with superimposed static stresses / 1
Y 3.N 21/5:6/3496 Flight testing by radio remote control - flight evaluation of a beep-control system / 1
Y 3.N 21/5:6/3497 Summary of results of a wind-tunnel investigation of nine related horizontal tails / 1
Y 3.N 21/5:6/3498 Exploratory investigation of an airfoil with area suction applied to a porous, round trailing edge fitted with a lift-control vane / 1
Y 3.N 21/5:6/3499 Calculation of the supersonic pressure distribution on a single-curved tapered wing in regions not influenced by the root or tip / 1