Call Number (LC) Title Results
Y 3.N 21/5:6/3277 Space heating rates for some premixed turbulent propane-air flames / 1
Y 3.N 21/5:6/3278 Attenuation in a shock tube due to unsteady-boundary-layer action / 1
Y 3.N 21/5:6/3279 Effect of phosphate coatings on temperature of metal parts exposed to flame environments / 1
Y 3.N 21/5:6/3280 Electrical analogies for stiffened shells with flexible rings / 1
Y 3.N 21/5:6/3281 Intergranular corrosion of high-purity aluminum in hydrochloric acid. 1
Y 3.N 21/5:6/3282 Intergranular corrosion of high-purity aluminum in hydrochloric acid. : 2- Grain-boundary segregation of impurity atoms / 1
Y 3.N 21/5:6/3283 Aerodynamic forces, moments, and stability derivatives for slender bodies of general cross section / 2
Y 3.N 21/5:6/3284 Examination of the existing data on the heat transfer of turbulent boundary layers at supersonic speeds from the point of view of Reynolds analogy / 1
Y 3.N 21/5:6/3285 Section characteristics of an NACA 0006 airfoil with area suction near the leading edge / 1
Y 3.N 21/5:6/3286 Generalized indicial forces on deforming rectangular wings in supersonic flight / 1
Y 3.N 21/5:6/3287 Heat transfer from a hemisphere-cylinder equipped with flow-separation spikes / 1
Y 3.N 21/5:6/3288 On the analysis of linear and nonlinear dynamical systems from transient-response data / 1
Y 3.N 21/5:6/3289 The minimization of wave drag for wings and bodies with a given base area or volume / 1
Y 3.N 21/5:6/3290 On the minimization of airplane responses to random gusts / 1
Y 3.N 21/5:6/3291 Experimental investigation of notch-size effects on rotating-beam fatigue behavior of 75S-T6 aluminum alloy / 1
Y 3.N 21/5:6/3292 Influence of exposed area on stress-corrosion cracking of 24S aluminum alloy / 1
Y 3.N 21/5:6/3293 Cumulative fatigue damage of axially loaded Alclad 75S-T6 and Alclad 24S-T3 aluminum-alloy sheet / 1
Y 3.N 21/5:6/3294 Friction study of aircraft tire material on concrete / 1
Y 3.N 21/5:6/3295 Effect of pressure on thermal conductance of contact joints / 1
Y 3.N 21/5:6/3296 Separation, stability, and other properties of compressible boundary layer with pressure gradient and heat transfer / 1