Call Number (LC) Title Results
Y 3.N 21/5:6/3252 Description and preliminary flight investigation of an instrument for detecting subnormal acceleration during take-off / 1
Y 3.N 21/5:6/3253 Some effects of exposure to exhaust-gas streams on emittance and thermoelectric power of bare-wire platinum rhodium. : Platinum thermocouples / 1
Y 3.N 21/5:6/3254 Determination of flame temperatures from 2000 to 3000 degrees K by microwave absorption / 1
Y 3.N 21/5:6/3255 Shock-turbulence interaction and the generation of noise / 1
Y 3.N 21/5:6/3256 Experimental investigation of temperature recovery factors on a 10 degree cone at angle of attack at a Mach number of 3.12 / 1
Y 3.N 21/5:6/3257 Effects of chemically active additives on boundary lubrication of steel by silicones / 1
Y 3.N 21/5:6/3258 Investigation of Mach number changes obtained by discharging high-pressure pulse through wind tunnel operating supersonically / 1
Y 3.N 21/5:6/3259 Investigation of nickel-aluminum alloys containing from 14 to 34 percent aluminum / 1
Y 3.N 21/5:6/3260 Smoke study of nozzle secondary flows in a low-speed turbine / 1
Y 3.N 21/5:6/3261 A method for evaluating the effects of drag and inlet pressure recovery on propulsion-system performance / 1
Y 3.N 21/5:6/3262 Starting and operating limits of two supersonic wind tunnels uitlizing auxiliary air injection downstream of the test section / 1
Y 3.N 21/5:6/3263 Lift and moment equations for oscillating airfoils in an infinite unstaggered cascade / 1
Y 3.N 21/5:6/3264 Study of the momentum distribution of turbulent boundary layers in adverse pressure gradients / 1
Y 3.N 21/5:6/3265 Vaporization rates and drag coefficients for isooctane sprays in turbulent air streams / 1
Y 3.N 21/5:6/3266 Experimental evaluation of momentum terms in turbulent pipe flow / 1
Y 3.N 21/5:6/3267 Boundary-layer transition at Mach 3.12 with and without single roughness elements / 1
Y 3.N 21/5:6/3268 Shearing-stress measurements by use of a heated element / 1
Y 3.N 21/5:6/3269 Additional static and fatigue tests of high-strength aluminum-alloy bolted joints / 2
Y 3.N 21/5:6/3270 Effect of dissociation on thermodynamic properties of pure diatomic gases / 1
Y 3.N 21/5:6/3271 Thermodynamic properties of gaseous nitrogen / 1