Call Number (LC) Title Results
Y 3.N 21/5:6/3730 The interference effects of a body on the spanwise load distributions of two 45 degree sweptback wings of aspect ratio 8.02 from low-speed tests / 1
Y 3.N 21/5:6/3731 Tensile properties of Inconel and RS-120 titanium-alloy sheet under rapid-heating and constant-temperature conditions / 1
Y 3.N 21/5:6/3732 An investigation of vertical-wind-shear intensities from balloon soundings for application to airplane- and missile-response problems / 1
Y 3.N 21/5:6/3733 Probability and frequency characteristics of some flight buffet loads / 1
Y 3.N 21/5:6/3734 Turbulent-heat-transfer measurements at a Mach number of 3.90 / 1
Y 3.N 21/5:6/3735 Bending tests of ring-stiffened circular cylinders / 1
Y 3.N 21/5:6/3736 Poisson's ratios and volume changes for plastically orthotropic material / 1
Y 3.N 21/5:6/3737 The motions of rolling symmetrical missiles referred to a body-axis system / 1
Y 3.N 21/5:6/3738 Theoretical and experimental investigation of the subsonic-flow fields beneath swept and unswept wings with tails of vortex-induced velocities / 1
Y 3.N 21/5:6/3739 Flight investigation of the performance of a two-stage solid-propellant Nike-Deacon (DAN) meteorological sounding rocket / 1
Y 3.N 21/5:6/3740 Preliminary wind-tunnel tests of triangular and rectangular wings in steady roll at Mach numbers of 1.62 and 1.92 / 1
Y 3.N 21/5:6/3741 An investigation of the loads on the vertical tail of a jet-bomber airplane resulting from flight through rough air / 1
Y 3.N 21/5:6/3742 Tensile properties of HK31XA-H24 magnesium-alloy sheet under rapid-heating conditions and constant elevated temperatures / 1
Y 3.N 21/5:6/3743 An optimum switching criterion for a third-order contactor acceleration control system / 1
Y 3.N 21/5:6/3744 Supersonic flow past nonlifting bumped and indented bodies of revolution / 1
Y 3.N 21/5:6/3745 Transition-flight tests of a model of a low-wing transport vertical-take-off airplane with tilting wing and propellers / 1
Y 3.N 21/5:6/3746 Initial results of a flight investigation of the wing and tail loads on an airplane equipped with a vane-controlled gust-alleviation system / 1
Y 3.N 21/5:6/3747 Equations and procedures for numerically calculating the aerodynamic characteristics of lifting rotors / 1
Y 3.N 21/5:6/3748 Calculation and compilation of the unsteady-lift functions for a rigid wing subjected to sinusoidal gusts and to sinusoidal sinking oscillations / 1
Y 3.N 21/5:6/3749 Torsional stiffness of thin-walled shells having reinforcing cores and rectangular, triangular or diamond cross section / 1